Additional display functions and section 6 draft done

2022-02-20 22:10:56 -07:00
parent 472662fb60
commit 700f7e28cf
169 changed files with 810 additions and 944 deletions
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+archive/EJS_2021-10-18T20:47:50.889/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 2500.0 kg
+Launch Date: 1978-12-12T22:48:52.804
+Launch V∞: [-6.090674217377611, 1.9365075336539337, 1.0648698904498797] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [-8.599568746419632, -3.929372774157513, 0.1598903162745283] km/s
+	V∞_out: [-6.29056111779008, -7.057496301214243, 0.189430044733671] km/s
+	time of flight: 1.3001684481349075e8 seconds
+	arrival date: 1983-01-25T18:36:16.804
+	thrust profile: [-0.07182664298936688 0.128593568038591 -0.0033731058601866584; -0.14496107486527016 0.019614663086595964 0.02700523476161058; -0.13805876571863734 0.22325211754031515 0.03286029056788893; -0.17816900109274997 0.3251881445829037 0.026780130823303633; -0.22091107053429537 0.2939652059103152 0.02344625079888415; -0.27021273578828064 0.3157707067103706 0.018476680775103425; -0.2836608580283999 0.3243901487958754 0.015956599062449752; -0.3068360438420818 0.3146860091819841 0.0105723882044705; -0.3292810606612484 0.2614007348524486 0.011754997912609486; -0.3082411232182887 0.3134585084987598 0.008638675487315959; -0.297477035499811 0.30298229839173424 0.007719364078028531; -0.2792458876097137 0.3365612134567308 0.0030760946585793487; -0.258013515008698 0.37181605254571776 0.0004414745677813128; -0.2544523802682347 0.3715892022148914 -0.002580647114731062; -0.25454731772339645 -0.17483362316511744 -0.005883918133923767; -0.1796298761984978 0.5543153441790251 -0.00479484757918334; -0.2058369839110801 0.6080531163079873 -0.006906018619479969; -0.19004325562362873 0.6808585182089864 -0.009561736441712605; -0.1156266736949098 0.7521324633143932 -0.011693074775341903; -0.1646635596394762 0.8059683170508395 0.00032177160211023075; -0.34106311540166234 0.8494504664186264 0.002611333186690262; -0.574056928115951 0.8481842537670797 0.020781891735754555; -0.8504461432226509 0.802093007453938 0.038642246376885334; -0.9757393021109353 0.6859427712453762 0.03010759580450199; -0.910154619484354 -0.2856020498446429 0.02716626068427377; -0.9506606524316868 -0.4220629222045593 0.026588482527997382; -0.8940323246940235 -0.4885156512655276 0.025659522671583713; -0.871711815021978 -0.6366970805623916 0.027252438491805468; -0.7825130410206668 -0.7886223488492162 0.024552574469084047; -0.6423866382660135 -0.9641690712998562 0.01943923061481833; -0.4222746446049146 -0.7552240852122724 0.02104985903045484; -0.31243361106519557 -0.6924455810440898 0.02009103653476697; -0.17694847513237855 -0.6163800718464629 0.01713953217130396; -0.08474393978779993 -0.5248074578000367 0.014833855045531795; -0.011864029086410653 -0.41157173573980044 0.010833647732578751; 0.04375646538299241 -0.3339499812330887 0.0102437227818524; 0.09877074621913506 -0.26063131652869664 0.007540144984536212; 0.14317962908971194 -0.13705579087085998 0.00457514684109456; 0.1878724827694389 -0.03413240870864257 0.001413559114121998; 0.22599292462070616 0.057490943926461244 -0.0017707613684488353] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [-2.476634908679025, -0.7638403672431561, 0.12353805637636839] km/s
+	V∞_out: [-4.768990627177744, -4.534467376403681e-5, 0.10167896839279073] km/s
+	time of flight: 3.658770760786993e8 seconds
+	arrival date: 1994-08-30T11:07:32.804
+	thrust profile: [0.006471497743567286 0.07106497737428204 -0.008140471536198022; 0.004995733058166156 0.052873900980690045 -0.007899436338773876; 0.004272642491454467 0.0419458983981252 -0.007586690700958719; 0.004973116708873848 0.031381901058011946 -0.006542654758388549; 0.00536350847874341 0.0273013528301513 -0.006176587202041747; 0.007518590340367018 0.02169288775473648 -0.00528877031336399; 0.0036238557416728152 0.016495952794332254 -0.0022638308531011276; -0.00010958570398813427 0.008959786487121398 -0.00432598221560573; 0.009954117506488221 0.014513865203024322 -0.0035592210115808817; 0.013845137512168095 0.012821565696435517 -0.003501423506019165; 0.013566725842853098 0.009425628557041911 6.270036523657755e-5; 0.017783414987452142 0.009855984645345286 0.0021753772096844526; 0.019489566460106304 0.012354329709679047 0.005793548267683204; 0.021683578221219416 0.01811719631055355 0.003762608782500969; 0.017079096209080324 0.016144776474641926 0.007911284545212918; 0.012398082206167794 0.020076808713162787 0.008106716953454938; 0.008762401768299392 0.02440897942380195 -0.002005437210534878; 0.00514400015849574 0.023138690993482515 0.0010057321378627475; 0.003365128336027771 0.015148288193322219 -0.00018639313635477017; 0.0061344497737247355 0.016694588916715065 -0.004287083697264384; 0.012554823998307069 0.0062789539468902575 -0.009651722283077235; 0.01605670030795382 -0.008038264781128481 -0.005237031814465953; 0.023192647642534668 -0.005570575659121995 -0.008994673684542912; 0.04612928562755005 -0.010719991611393014 -0.0008023672732823759; 0.05858401720072217 -0.010979829491959435 -0.008059079622404293; 0.05701510663734706 -0.010301033182780462 -0.012816132735822279; 0.12857486218229078 0.012127084380242403 -0.007019589997056743; 0.07046066566571119 0.00464970978335277 -0.011672809507840227; 0.03985428527436419 -0.0019924367728197186 -0.012558591331338576; 0.06686858365944223 0.005678621891433029 -0.010903627408032808; 0.07367343491763058 0.009741112752589848 -0.010704279529209966; 0.07537733671151621 0.01674670940193965 -0.008867677839006596; 0.07633627415854556 0.019150669506264345 -0.008451317304137626; 0.07643409034436661 0.02155849875895805 -0.007849984660028087; 0.06985438673831253 0.022966208001301266 -0.005766712290140227; 0.17223276598864495 0.025568128921766423 -0.005966844719858575; 0.07370003423403078 0.025553875486905096 -0.005522050157923093; 0.06883339474564308 0.02563737571090785 -0.00448206392796866; 0.06299408118929155 0.024637846056827617 -0.003527665672570326; 0.06334286110038836 0.025139861032886325 -0.0028843365012048176] %
+
+Mass Used: 765.4852928443993 kg
+Launch C3: 41.98032173371355 km²/s²
+||V∞_in||: 2.5946934749389903 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EJS_2021-11-10T17:39:50.182/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 1977-06-03T12:59:37.799
+Launch V∞: [2.037663352777953, -8.43490917599047, 4.662061679317432] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [2.0543036098784477, -9.13281943510734, 0.46707958098685376] km/s
+	V∞_out: [-9.062292345569814, -2.3925561030248113, 0.012115863710008418] km/s
+	time of flight: 2.651327999769022e8 seconds
+	arrival date: 1985-10-28T04:59:36.799
+	thrust profile: [-0.3666137901495707 -0.46957429211809487 -0.06095376292954174; -0.4665558706644106 -0.10394413351183696 0.28610656396587303; -0.4953660695905247 0.24271134488915128 0.26741901645132793; -0.5238470521312512 -0.14904137588352487 0.11667074352725965; -0.3130301366808927 -0.5555434925364752 -0.06526933016356705; -0.5423650979399098 -0.5620740091733915 -0.20854153512243992; -0.5246082788630371 -0.5025978253322431 -0.21135002916159024; -0.5697267878022093 0.06321816977663988 0.22886544507082332; -0.6120311447829342 0.412763321448428 0.15616795632012262; -0.6539149704504248 -0.4641829118760538 -0.12954694971592742; -0.20129129722008116 -0.6165039554386057 -0.13481895080818976; -0.3977328905362448 -0.5756437901430289 -0.1442400227486695; -0.41396000033260266 -0.4597767223691828 0.014956812046032929; -0.5419266443658755 -0.3913185005375316 0.10340560958225044; -0.653821761083701 0.0029065521912539248 0.1254968793250296; -0.7392954157600166 0.41739296978429474 0.048387346920351154; -0.2993155496706189 -0.862564466919382 -0.18789013527425982; 0.54061683054975 -0.6077177484151901 -0.38511905650494493; 0.3595047789991687 -0.26996788568129604 -0.058521775645983334; 0.6079025381989944 0.7866364488796997 -0.002816798435360894] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [-1.5527277061928566, -9.290875340376942, 0.043699679303627025] km/s
+	V∞_out: [-0.7664706270913678, 0.08215083439603876, 0.01420153594858485] km/s
+	time of flight: 1.4356440000946072e8 seconds
+	arrival date: 1990-05-16T19:59:36.799
+	thrust profile: [-0.45363346920243913 0.007414553001916338 0.024833395801696717; -0.42929594280033395 0.029217209524867983 0.025014737699506233; -0.40759184786564384 0.06351691143576771 0.02515016106459692; -0.39712301899974733 0.12845858528432538 0.022572693508776966; -0.4009114657635113 0.21043524639923297 0.029274749214758526; -0.45017496865976625 0.2843178178382748 0.03516955271197208; -0.6353367593618829 0.007373393962796029 0.061015069673970156; -0.17636211915789957 -0.5399824298560856 0.046019016312036976; 0.10022826993820261 -0.4452055922359326 0.005465675250313729; 0.12030211019389436 -0.30664235607958396 -0.014741914655282726; 0.13606528305073498 -0.24140989738984756 -0.01809230195253888; 0.14886416528008864 -0.14793802290529368 -0.024870924926003683; 0.1573360419373063 -0.037299267927507894 -0.0326622325810398; 0.15533491321993567 0.08595709158871023 -0.03599171154371347; 0.1456345166609902 0.1981225994755318 -0.03517653838413347; 0.1357020340234525 0.2942201982026304 -0.033486517711519836; 0.12603250981007186 0.3753587231244459 -0.031672415654865504; 0.11656119662828038 0.4425819361389264 -0.030365847244885866; 0.1075278998670041 0.4980664219019285 -0.02910770547729163; 0.09630035393180529 0.5468861781276572 -0.02846997433085122] %
+
+Mass Used: 1956.4800896757313 kg
+Launch C3: 97.03458384822258 km²/s²
+||V∞_in||: 9.419832141921349 km/s
@@ -0,0 +1,36 @@
+archive/EMJS_2021-10-18T22:47:27.423/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 2500.0 kg
+Launch Date: 1978-01-03T10:43:56.684
+Launch V∞: [-3.9272284612384682, 1.103272773876818, 0.5261327502187312] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-4.302171521788235, -0.9224228322302193, -1.14321961684719] km/s
+	V∞_out: [-3.884897307404638, 2.338666041291152, -0.3214778995965392] km/s
+	time of flight: 4.342577286549467e7 seconds
+	arrival date: 1979-05-21T01:26:48.684
+	thrust profile: [-0.013447144151271642 -0.03768936107210863 -0.016368572374325367; -0.011844904106064317 -0.02655981602735897 0.04457863849948758; 0.004072854216357777 -0.06638130237888651 0.08240263777419533; 0.02275688493856809 -0.11176740369554655 0.10543301498940685; 0.045760812777573635 -0.1494893115542728 0.13159970546846236; 0.07695648098710427 -0.2178829328468449 0.16954108284269187; 0.13157259005460648 -0.23862770794850882 0.20680275357201225; 0.20764505272897338 -0.2465698722765297 0.20163109585168845; 0.269333209504411 -0.2588680411909609 0.21321916585564238; 0.32998447568721123 -0.2680930176939294 0.21619301937830762; 0.37620045883152436 -0.2724317467650694 0.21675621863459776; 0.4323971239602839 -0.27348332645907797 0.21102218660275301; 0.4703186634081572 -0.2708338296152373 0.2048610047676473; 0.3597048908164455 -0.30168467216940215 0.22271019411557225; 0.5595433516897296 -0.2520380850567037 0.17984221224819918; 0.5791156404967587 -0.23718296966437183 0.16719173939790813; 0.5889605820654115 -0.21609542430924483 0.1537220766009391; 0.6205968306722238 -0.17806607765297935 0.1316941071277918; 0.6524073886741711 -0.12692115399236642 0.11004853364521734; 0.6460698541874085 -0.07099707280996082 0.09067420762823987; 0.6589965680731105 -0.0011913829014568824 0.06930838130612939; 0.6644670925985161 0.07766081746348873 0.047739690615405714; 0.6638056516192694 0.15460246981984838 0.022788460359890444; 0.6487320139399378 0.23540643458585594 0.006175068126340953; 0.6410891380475499 0.30957574688150136 -0.024675224595270474; 0.6596012529020187 0.3635711825364716 -0.05037652503759746; 0.6519587145862431 0.4348113869832688 -0.07440654083355334; 0.6396145955395663 0.4869696665250608 -0.09620744743991923; 0.6245682796976347 0.5293874600823794 -0.11775697968922781; 0.593910582743051 0.5588159151044279 -0.13836508084578183; 0.574924822237447 0.595859442758361 -0.1580408539927286; 0.5381088810773483 0.6184991449662873 -0.176595552415949; 0.4870762683434131 0.6412890605468125 -0.19413030906155615; 0.439283105198052 0.6567497136482087 -0.2099817083731474; 0.3905046740712172 0.6771957181192864 -0.22402603882218294; 0.33610274686846303 0.6788473071682596 -0.23595909126049985; 0.3207666874572572 0.6870614251927035 -0.24540652759693637; 0.3333226555463708 0.6821940503695704 -0.2524119839204476; 0.33988184850576236 0.6948528069143785 -0.25798146577000974; 0.262156668632568 0.6629465563176469 -0.25755720204185983] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-6.271665555774167, 2.489880381632231, 0.2737481121245321] km/s
+	V∞_out: [-6.328712914963172, -2.269617219606894, 0.6361021725151511] km/s
+	time of flight: 7.391542374612738e7 seconds
+	arrival date: 1981-09-22T13:30:31.684
+	thrust profile: [-0.651702750704448 0.9073386122566174 -0.15302324645504992; -0.8436259115068814 0.8846871422239923 -0.1430997495310651; -0.9267854449167796 0.8312863450886124 -0.13511100758509673; -0.9600707304615784 0.740006968040963 -0.11491212977710746; -0.970657142239052 0.6072438527833685 -0.08715957534996058; -0.9690338392067889 0.4496492582625218 -0.05678572955291726; -0.9648702460776198 0.3036294954888355 -0.02831453482454512; -0.953439675535875 0.1905302687136827 -0.00953486298802024; -0.9341753371455765 0.12376645574107052 0.0075361709404562416; -0.9007180283411284 0.11288944124619768 0.020682328021608187; -0.8535366782383068 0.12318780763193395 0.02992218095903821; -0.800117702784335 0.13563803244119918 0.037009416032617766; -0.7424998976132356 0.14417025911089032 0.04304690047119499; -0.6807950776764372 0.14681090073476885 0.04617975331606857; -0.6328612925369842 0.15152680757881914 0.04977126226308689; -0.5610970976842719 0.15467315146782326 0.05350620192819169; -0.5025226368250042 0.18566706623414964 0.053295836945406745; -0.44534221042427413 0.2027168105831806 0.06028616190776899; -0.3910508537425582 0.21346977680504767 0.06272206611662426; -0.33824274812686217 0.21151203999512455 0.05844884652618134; -0.2879273094401357 0.22205558075545428 0.062044056311167294; -0.23986751786072552 0.21244080317292385 0.05794789870068873; -0.19545403904499187 0.20829143417885157 0.05688223757206132; -0.1527545543555382 0.1978561892546842 0.05623011131828713; -0.11559604827592482 0.18490191395766567 0.05524562653659965; -0.08095336618391784 0.17429659576325035 0.05454473224761285; -0.04333857765170937 0.15701791263228007 0.053169386805572795; -0.022342840863649856 0.1470817213022724 0.05164766449120743; -0.010613815457526017 0.13407442987582807 0.05609742282316187; 0.014056122303914778 0.12003333630129563 0.04747259995547432; 0.025229791437383145 0.10377059466112984 0.04428337400788782; 0.029712683447225913 0.09559188789585858 0.04082772777508522; 0.03029438904709797 0.07431757850700871 0.038278807305194715; 0.029722009787300635 0.05930702273250002 0.0348540851806576; 0.01593715470840344 0.044674331509385615 0.028967415183582586; -0.000492442005028769 0.031200772293903677 0.020993671074642267; -0.006234987537495302 0.018996220064454866 0.018738102077466796; -0.011913350640564655 0.015029637114641062 0.01635980608027226; -0.0052952509645315905 0.016962720377167385 0.010862908397557422; 0.011554684289671836 0.009513907349519868 0.015590729291820548] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-2.66193677884025, 0.3493623501269433, 0.09631489633962698] km/s
+	V∞_out: [-1.3635159497610903e-6, -1.7426433396047956, -4.029575055523134e-6] km/s
+	time of flight: 2.923160019123397e8 seconds
+	arrival date: 1990-12-27T20:23:52.684
+	thrust profile: [-0.09565536202858775 -0.015035898430190172 -0.009725454256544613; -0.07897261343020702 -0.00238009948978215 -0.012117445455209819; -0.06645206939288806 0.008636439223724948 -0.014851318729266058; -0.05449812297361354 0.017907615130034197 -0.016656566536618823; -0.04676491594747234 0.0238064540531044 -0.019059516117866073; -0.039312625773118844 0.028739205371698107 -0.020706756033790515; -0.032508673986867166 0.030839694787733306 -0.02231126078139291; -0.026215833742130597 0.03418636767869463 -0.024419438602774776; -0.020025215586652084 0.03409752332243777 -0.023732100596602256; -0.014680807032132858 0.03419653726235092 -0.024327004616712264; -0.009588993073309765 0.033353213352348796 -0.025065865289011502; -0.004081331343615601 0.032206257965477735 -0.025284019620742403; 0.004436085441904554 0.03004281047196769 -0.025518080838194724; 0.003852155931769067 0.028868654208565277 -0.025034955622429116; 0.014595311279665475 0.024689069764230968 -0.024125952742839546; 0.023835030598535523 0.01937393285043024 -0.022789732691328064; 0.028768977010652057 0.01487895745065578 -0.020764405371729064; 0.03449379075433154 0.009167522926912489 -0.017310390463345503; 0.03887773174976339 0.0016135769473159282 -0.012795043007529138; 0.03948791694275722 -0.0054235445608209094 -0.007468721949686625; 0.03604210919888823 -0.009633435044280795 -0.003200192885088548; 0.03443106112767494 -0.017570509450106714 0.00031994757386726437; 0.023453704505205238 -0.02322162963098838 0.00694117337721031; 0.0078124435105612735 -0.025361557923029746 0.009670326612974586; -0.007009828221787631 -0.019142856544318344 0.005952252240702955; -0.0022289327086480984 -0.015568008089639247 0.01086887386460354; -0.009421778778551666 -0.0010457741968390834 -0.002407687921706048; -0.0035517830401844896 0.0018240199199404793 -0.0040160718149752405; -0.002129254138139583 0.002718055520037271 -0.0042655270001592804; 0.0050176954376301 0.003517635186843921 -0.006015994949785137; 0.012147363410032091 0.0012973665370782572 -0.005458560115787976; 0.01776111522887621 -0.0016117554359792092 -0.004000987096420474; 0.023135602956962306 -0.004915462816984336 -0.002315765154245354; 0.027947730240507136 -0.008258729820534555 -0.0006692523877146306; 0.03432392602635945 -0.019679422262737983 0.0010690598828892513; 0.03507829451962251 -0.01564402182826511 0.0028875147856150364; 0.03946622337950674 -0.017170102864219668 0.004665855593504292; 0.043736859810655476 -0.020187590939023437 0.006180816259617711; 0.04718123250986514 -0.022930289449652832 0.0073607552727975875; 0.05166943118533454 -0.025839010876439632 0.00838475645697907] %
+
+Mass Used: 594.0545609036042 kg
+Launch C3: 16.917149871192045 km²/s²
+||V∞_in||: 2.6864917691080947 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-10T17:54:03.858/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 1977-07-15T09:14:38.873
+Launch V∞: [2.5147318268598355, -1.1103623444144004, -6.402642134012201] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [1.4161036678756145, -1.1612060546662615, 2.9720800484503234] km/s
+	V∞_out: [-0.90804226462538, -3.0734160134493123, 1.3849536778316178] km/s
+	time of flight: 8.105040003981963e7 seconds
+	arrival date: 1980-02-08T11:14:38.873
+	thrust profile: [0.627838637604648 -0.12503628432096117 0.7855611132388014; -0.5289458287476022 0.6777841575676512 0.7075837038292085; -0.2373838703336668 0.7909345611869171 0.4331633366544985; 0.5432353517595965 0.7768839631178791 -0.783167310773754; 0.5396869301168233 0.7683167946626912 -0.7571970728573518; 0.23588696621684396 0.7769451734643089 -0.7270972946851668; -0.7694041770581667 0.601335658849241 -0.6637596322235111; -0.7921780190588894 -0.600905356962876 -0.44048431937604654; -0.7622543155226738 -0.7373700209872003 0.7911418295324951; -0.6606019028334599 -0.7987421962324748 0.7323144603647144; -0.1388661271934692 -0.7740008599199898 0.8060677773780438; 0.6499414579435336 -0.7130596280638938 0.7498586673145985; 0.817143568445207 -0.36590025267892895 0.3893357714242182; 0.7221677618564997 0.7956815784628078 -0.8027852216637569; 0.35730904625294274 0.8181592617310386 -0.8193971102980425; -0.7933587691663879 0.791605697884167 -0.8000227654400738; -0.8367294372565426 0.7202574934137008 -0.7630351620402276; -0.8524884295875419 0.527782602224365 -0.6846066726355504; -0.8673603491643094 -0.809433634144834 0.39335608125780586; -0.8116407828303132 -0.8844460508958141 0.7943966816976175] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-6.284565742386362, -9.76715307446354, 0.5888918727291137] km/s
+	V∞_out: [-9.279749880105083, 6.689786284603497, 2.0909888468209963] km/s
+	time of flight: 1.1491560055966887e8 seconds
+	arrival date: 1983-09-30T12:14:38.873
+	thrust profile: [-0.9127396122468532 -0.9218277687731674 -0.4263668054485564; -0.9127835283943397 0.5076311793916051 0.6901653820507275; -0.9277032940195239 0.8072913628070539 0.7376714170725708; -0.9413418283270233 0.8224253560321766 0.7734378668742132; -0.9475800103183779 0.7633312809013366 0.7988746215077034; -0.9543633564369559 0.47787598052458224 0.8062149670969349; -0.9559692329051825 -0.8194886763245005 0.5560168723764345; -0.9513976484586338 0.33441960267381193 -0.13333116315754445; -0.9427922092415756 0.8485944388724405 -0.37802038562147244; -0.9554914463244739 0.9253215472599327 -0.6472191305079521; -0.975933074552162 0.7725813929691159 -0.7667329121636777; -0.9712483448360393 -0.9635899350612177 -0.5468548163709348; -0.9443483595384782 -0.9692759844140697 -0.28668950342079663; -0.8886926888299911 -0.964158515619833 -0.20020199822347967; -0.7777727089323969 -0.9583099186800864 -0.17642040634769085; -0.5484454199881573 -0.9475574807265811 -0.16061558441899781; -0.16145042784627028 -0.9295820744714413 -0.14398087412630792; 0.1489729267980805 -0.8875509875058407 -0.12186518694197303; 0.3863989762520739 -0.7243671949614064 -0.10506111941783687; 0.550866374411865 0.6515340599054279 -0.09506697653138528] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [5.425276900065363, -6.401959760024709, 1.628957215805309] km/s
+	V∞_out: [-2.078410685140159, -3.155305729801939, 0.0008586072596457413] km/s
+	time of flight: 2.122127999843037e8 seconds
+	arrival date: 1990-06-21T16:14:37.873
+	thrust profile: [0.4137213553359692 -0.3123419166895793 -0.07413066083839148; 0.3866860426238052 -0.22444859437512898 -0.06473683963171227; 0.31555810889484437 -0.16704122103878502 -0.05672742473286491; 0.22729716039326592 -0.12827357453673835 -0.031539395787956954; 0.143207212399456 -0.12782196637060753 -0.020925701304977146; -0.055315287904767946 -0.1596070863670293 -0.15698789612711658; 0.0855670371677483 -0.3691654213130422 -0.22727650425327833; 0.296362079592094 -0.36205016550808794 -0.08720444491924713; 0.3416336893889104 -0.37382177982174647 -0.05355021694096375; 0.3922447283373164 -0.35961171719778656 -0.03138748595138845; 0.4272895758116155 -0.3267679698520526 -0.017497312957446522; 0.4465876315319068 -0.2826782360645849 -0.008534675888530218; 0.4531265921438839 -0.2323243789797917 -0.002376606148144884; 0.4495616785265872 -0.18074814564085967 0.0023041257879340494; 0.4380764579262854 -0.1330536192097116 0.005943447204693447; 0.42071889349085684 -0.09344905521564274 0.008645824111706685; 0.3990398415062969 -0.06332998130635517 0.011593397065563935; 0.3717084241277894 -0.04056062633087571 0.0157282909739208; 0.33657096418837157 -0.017725329809315477 0.03801942779075905; 0.32630435662337576 0.0002709235371287296 0.033211487884096974] %
+
+Mass Used: 2627.443374929516 kg
+Launch C3: 48.55060699314355 km²/s²
+||V∞_in||: 8.548229045965172 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-10T18:46:26.719/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 1977-08-28T19:16:48.911
+Launch V∞: [-0.9048124421086198, 1.9143247567671402, 1.0655764532581016] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-2.4343783407486486, -4.687961859367619, -2.933139307760753] km/s
+	V∞_out: [-4.790214200771935, -2.8588778216214474, -2.321748592254448] km/s
+	time of flight: 1.2520840640242675e8 seconds
+	arrival date: 1981-08-16T23:23:34.911
+	thrust profile: [-0.6224581879584439 0.4288059372368617 -0.369846309902295; -0.8456103096731954 -0.5449676132404117 -0.5207697451591612; -0.8002461593492456 -0.855950096213463 -0.3124435417439843; -0.08909026312356522 -0.8654901195188492 0.07012982568146232; 0.680001252515441 -0.7588164444715032 0.36639076258430675; 0.5600241806519821 -0.5524736520531364 0.42732020550718447; 0.16764662042831702 -0.38130964149055036 0.34119753879891973; -0.731954705851045 0.09173304239444241 -0.3217028849043164; -0.8708852593282298 -0.20046295640353465 -0.47555463513488316; -0.8714792916879354 -0.8774730456609726 -0.40411815736943946; -0.7503507155222385 -0.8995426849328464 -0.19904254786993072; -0.21243617845242554 -0.8809796651748026 0.05347795073943726; 0.6472006222755674 -0.8484331643135395 0.11021347676692661; 0.7443657429086448 -0.7955146419656197 0.23886041656554424; 0.7440649663077856 -0.6390085790476502 0.3042575860828415; 0.37484890774561835 -0.37162261741629815 0.19144601961385382; -0.3550450393056071 -0.11435230249867454 -0.07617629787736838; -0.9195229993807225 0.2789170446342234 -0.2615678112840567; -0.9727616469871604 0.3446917247288234 -0.257471197235714; -0.9808492088715268 -0.5477259908772488 -0.44853687745916715] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-6.701136691962909, -8.599974967150617, 1.3162577103992203] km/s
+	V∞_out: [-7.466152781006179, -7.773882414996021, -2.1024987830209496] km/s
+	time of flight: 5.836177608302693e7 seconds
+	arrival date: 1983-06-23T10:59:50.911
+	thrust profile: [-0.9775204977097908 -0.5214058341481157 0.16197437982089447; -0.9681501773489387 -0.7500057879390385 0.22817317938497259; -0.9525762370469925 -0.832426651123316 0.28200011488079785; -0.92761259022897 -0.8555389932740242 0.3222489903321434; -0.8871450236047153 -0.8560245708679001 0.3479490816123863; -0.8195685407028787 -0.8487998122656493 0.3566147862452735; -0.7790460014892773 -0.8311841138895902 0.3582600049182118; -0.6190731426200151 -0.8078635763142238 0.3511260288381265; -0.5145129727216806 -0.7780683585790256 0.33770986872031583; -0.4148838449023785 -0.7435111238696445 0.29665258639127334; -0.328030995132986 -0.7010614327842398 0.2948502276631388; -0.2661376870905083 -0.6524456881612392 0.26648173671933306; -0.21007010595989548 -0.5926356418988066 0.23592936608072115; -0.16014790791450959 -0.5250602978661468 0.2043260162059496; -0.11439806841436284 -0.445002817701425 0.16965789733717526; -0.07922096702487279 -0.35121979340219833 0.13666559998803526; -0.04342546734347377 -0.24958467169576376 0.1009510992394805; -0.009561808725198587 -0.14116721656848708 0.06776342231966652; 0.025698079008218886 -0.029169079250700856 0.03660047680102405; 0.06723364775247613 0.09468227499819452 0.007603348452937278] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-4.879936875669879, -0.47223217562047437, 1.5644706826898132] km/s
+	V∞_out: [-0.004764406068025241, 3.023809215796096, -0.006813540558789842] km/s
+	time of flight: 2.520438083264169e8 seconds
+	arrival date: 1991-06-18T15:09:58.911
+	thrust profile: [-0.09400215473661182 -0.18945521309217062 0.1271918910889239; -0.08607974390576098 -0.15730289401708353 0.1330350509096681; -0.07832275239134029 -0.13478208666438357 0.1351441081454202; -0.07132837621235137 -0.11668356299904072 0.13473290589837142; -0.06422308680008934 -0.10329018345067097 0.13124190941207606; -0.05483219880785128 -0.09065397169544913 0.12875633044650717; -0.04534456797231015 -0.07960292266050767 0.12395016513276043; -0.0352252711827991 -0.07015964172632169 0.11766514477500203; -0.02415557927465716 -0.06150640906378341 0.11072639537362276; -0.012611759737086297 -0.05352376356987194 0.1025041600979924; -0.0005755408110000229 -0.044830667850551016 0.09493441557954609; 0.019044842896509144 -0.04345125363942511 0.07403861776967349; 0.02592414982088686 -0.030002827924179683 0.0741211457115302; 0.0402832985262284 -0.023419092869979216 0.061815224815860395; 0.054217569381438825 -0.015792813536919307 0.048795971971107605; 0.06660233013037975 -0.008291406855245277 0.03513209811142393; 0.07850378454520773 -0.0026815097750121706 0.021588614394289437; 0.09131650833507947 0.002815289108732593 0.005218753137309239; 0.1023654635811782 0.007548514976676589 -0.010865691913744062; 0.11263768787148964 0.01184198808791625 -0.025804576648942177] %
+
+Mass Used: 1595.0391476343098 kg
+Launch C3: 5.6187780075042495 km²/s²
+||V∞_in||: 5.146295333073091 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-29T21:44:47.574/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-06-24T11:13:35.652
+Launch V∞: [4.204198767059533, -9.994451029411268, 4.407763020256069] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [1.1816902279242838, -9.996430420980913, -3.9141617445235055] km/s
+	V∞_out: [0.37910175293619774, -9.534044813617678, -5.060049667159223] km/s
+	time of flight: 4.577040007583382e7 seconds
+	arrival date: 2024-12-05T05:13:35.652
+	thrust profile: [-0.6281059032448896 -0.9645978361567867 0.04825409754226176; -0.8740723336039602 -0.9597496199427967 0.05604914227980348; -0.897647871256038 -0.9575735835349201 0.09800966403698955; -0.8947340470580677 -0.9548346668410663 0.15634176550887674; -0.8837997723274917 -0.9506389891549062 0.2119922535014052; -0.8733870717624931 -0.9429899204491616 0.2583708134992254; -0.8720845887317354 -0.9025764262000016 0.2931913647382538; -0.8825703424810087 -0.5611857908303168 0.31198994673950864; -0.8867206383135808 0.3805834562800023 0.28726172697464486; -0.8888991630049579 0.788013986816961 0.23249659162459266; -0.8970204827538024 0.8882296727690108 0.17207243243036158; -0.9065712428541088 0.9234064642311088 0.10537365025980958; -0.9148714632891286 0.9404349357133255 0.03442544496598595; -0.9208141256954919 0.9503791830745603 -0.03567082436670164; -0.9236394768970245 0.956949522940748 -0.09754989596668419; -0.9220273833669875 0.9618350488524434 -0.1430101775953111; -0.9126940508648808 0.9660194230411197 -0.16197775579747833; -0.8857853310494002 0.9701186203520745 -0.15061297758287906; -0.8029871986880408 0.9745861477536751 -0.10435361844832336; -0.4980925964808032 0.979366793392864 -0.011905648117825195] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-3.3293666105405575, -7.620971578491845, 1.0687733254722611] km/s
+	V∞_out: [-6.935603481721296, 3.497201324971365, -3.158033428514645] km/s
+	time of flight: 2.2417560002564985e8 seconds
+	arrival date: 2032-01-12T20:13:35.652
+	thrust profile: [-0.3656566194762257 -0.22912757683936658 0.045808165828645775; -0.5810293395224363 -0.29607251343651775 -0.13300805411577823; -0.4856402754635828 -0.4614047283645683 -0.18145385059581523; -0.2733529556486418 -0.42488777696168484 -0.1702396496601306; -0.06558140669038927 0.07510354553305262 -0.1674187982096823; -0.21526857860677945 0.45034604284055235 -0.04663600347350332; -0.4898784174638757 0.4672206097962957 -0.023748597462847795; -0.5650731143780724 0.15545877435880226 0.0018975633487120474; -0.5089407649543735 -0.33474815321731466 -0.08561486507950282; -0.41521030324056496 -0.34928781074095683 -0.1390599491503587; -0.3251150806058122 -0.22460933014070283 -0.1345228273672964; -0.21831464912318946 0.2614219842817418 -0.09124370704265022; -0.33671096662164174 0.5619362774706881 -0.03884229233090504; -0.6767648054832806 0.6334416704852173 -0.05037338528195778; -0.8062403423691754 -0.29179921474968684 -0.12036905303677174; -0.5776385810576635 -0.7669983678262886 -0.0642881827918457; -0.016220388338266608 -0.6010313543551327 -0.09290105482283402; 0.07029572715666328 -0.328415627959751 -0.11381534454303409; 0.08335842385908794 0.04906852415946227 -0.12154942027309859; 0.08187921283901471 0.3612744411676179 -0.11286850125684299] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.0842531035611531, 1.2406035825140813, -0.5854117544230216] km/s
+	V∞_out: [-0.023022631572720317, 0.023022631572720317, 0.00027223728207050724] km/s
+	time of flight: 4.927968000000019e8 seconds
+	arrival date: 2047-08-25T12:13:35.652
+	thrust profile: [0.35472737510521357 0.18207157177175717 -0.03254085314485865; 0.2266310259633882 0.3143675224006778 -0.01634653859009041; -0.10803902823003882 0.2896540320383328 0.03698624574214201; -0.11188790602824296 0.0915541039807244 -0.021159489070060124; -0.06936165955738366 0.05183112468149076 -0.057003976993703534; -0.04249032460536079 0.037075185269534884 -0.06367664972970241; -0.027648538697579345 0.023332194805352827 -0.05841953485870754; -0.014366139480565362 0.005827157994898504 -0.048061820566802686; -0.0022792620463178326 -0.009394651147162938 -0.03506791686081867; 0.009030269893451199 -0.02706297073989417 -0.024848503402645945; 0.019191776330403483 -0.040724325634559244 -0.013472336734798319; 0.03352802263728233 -0.0548449925970575 -0.0022387391078727108; 0.04758516117011756 -0.06820275602257245 0.010158607228174674; 0.06047608901522452 -0.08069030413927751 0.023475738159138497; 0.07126343200191616 -0.09274908219459146 0.03743668043976812; 0.0790452936746388 -0.10510006610579826 0.05145735407037108; 0.08312186020602563 -0.11864440821410976 0.06447591831670829; 0.08349578603424643 -0.1340449393883435 0.07445748197303119; 0.08231493768561268 -0.15058794815993298 0.08381258156479551; 0.08110239170439432 -0.1733639918710088 0.09588561948953665] %
+
+Mass Used: 2029.541947000274 kg
+Launch C3: 136.99271349498176 km²/s²
+||V∞_in||: 1.748544813193361 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-29T21:56:54.243/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-02-03T22:31:58.060
+Launch V∞: [-9.983658485652342, 5.052584189132008, 8.454011703658189] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-9.953421438043394, 3.213281933198845, -5.745066702073697] km/s
+	V∞_out: [-9.111152118008471, 4.863192665850899, -5.978278871452932] km/s
+	time of flight: 6.973930850639665e7 seconds
+	arrival date: 2026-04-21T02:33:46.060
+	thrust profile: [-0.9327909510849908 -0.5004864936548854 0.5880652125453542; -0.9029912019179394 0.5317310327031032 -0.479053583548179; -0.8739292812639873 0.6883047550245208 -0.5367631771071988; -0.8429685817072956 0.7298891216769086 -0.5130875244914932; -0.7976818801439988 0.7445652374517617 -0.43930087061099776; -0.7138755130219845 0.7567268126061615 -0.12248962250324259; 0.3962540499696817 0.7641554988596735 0.46486366383018496; 0.734311596231425 0.7455876887812815 0.47150616674759604; 0.8174592629690127 0.7463739223262722 0.5121440363573074; 0.8611866709577258 0.7575379533647393 0.5286900263176879; 0.8878359656973905 0.7764148245561391 0.5284942874419258; 0.9054328385770163 0.799696138207671 0.5134234416727862; 0.9175793861615414 0.8244011769369346 0.4786693481341792; 0.9260901378249389 0.8482781912744276 0.4059545252589148; 0.931827122595938 0.8695510665682376 0.27969911096378186; 0.9351654063561202 0.8873770941740391 0.0557896800207434; 0.9359855094240302 0.9011770122818098 -0.21365898834998476; 0.9338922411647969 0.910802339678919 -0.365757719064907; 0.9278284047571169 0.9146993842728531 -0.45267349649595484; 0.9177962416138067 0.9074601171998934 -0.48335462518998995] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-4.046083430194879, 6.572285306163753, 0.7499685576972142] km/s
+	V∞_out: [-6.445354159446693, 3.323503238892241, 2.745880595515267] km/s
+	time of flight: 6.991559948627624e7 seconds
+	arrival date: 2028-07-08T07:33:45.060
+	thrust profile: [0.5340118690878064 0.8946355483481895 -0.6067329080424446; -0.3678947664519958 0.8593146540157065 -0.5131755344574285; -0.39005831784853146 0.7991144657043887 -0.41508437369833046; -0.10776295134122015 0.7502923022084157 -0.3752944615562001; 0.17190209160722916 0.7255675171054287 -0.36441383578999126; 0.2980908476585895 0.7135279015946394 -0.35965213622497433; 0.3456788185986325 0.704810230513307 -0.3538631475411222; 0.3583977073758296 0.6949801520421466 -0.3447797296975572; 0.35356864150294026 0.6822744172223295 -0.3320858164407262; 0.33890034451249423 0.6658132457508765 -0.3160568300648956; 0.31830164408791184 0.6448711256196155 -0.29701300971671146; 0.29395968164603875 0.6185806040894148 -0.2752331841044432; 0.2672555928298822 0.5857596234549681 -0.25095251239959365; 0.23904121980768947 0.5447808233719543 -0.22439601711290494; 0.20994568191742563 0.4934318160029573 -0.1957402258157503; 0.18033604818385496 0.42882214377711125 -0.16518210760018237; 0.15047492443932542 0.34753119746438316 -0.13293973479266868; 0.12055531050530945 0.24650927403513742 -0.09927152610592575; 0.09086119930934154 0.1254331780451551 -0.06454483894976729; 0.061810968904553794 -0.011869676978603206 -0.028875376938032212] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.7080958958005663, 1.0532975410358802, -0.5234285178154677] km/s
+	V∞_out: [-0.042057638575385886, 0.01628965046711138, 0.0014262587493817428] km/s
+	time of flight: 5.410008000022286e8 seconds
+	arrival date: 2045-08-29T21:33:45.060
+	thrust profile: [-0.0006869622475465983 -0.05655873970732918 -0.08006272268398595; 0.003873967057859684 -0.05311730345001728 -0.07482636442553423; 0.006727479367092001 -0.04684548439756908 -0.06417959013850079; 0.008028763484199715 -0.039535927541232405 -0.04928157856745151; 0.007320491169929365 -0.0336280046809453 -0.02966715910096899; -0.005028754990363752 -0.02826953540745633 0.014881687165696877; -0.001695926581312149 0.007613100970810841 0.050070217801999904; -0.0023998275768972828 0.0206376998032102 0.06370073498988323; -0.006452242213360922 0.03719762725683077 0.06583225244312285; -0.05603050531565261 0.05854878555357484 0.025067239804525545; -0.09154744763319163 -0.03948563977311411 -0.03805667977702517; -0.05562816267322614 -0.08822935587386244 -0.06523679311574879; -0.024248131898468382 -0.09707814140258143 -0.07671757975959173; -0.0030870165238090197 -0.09430812478084437 -0.07870021435343663; 0.012035011271421321 -0.08691656821902476 -0.07510940925295292; 0.023445741439504515 -0.07733785582837824 -0.06757603737096467; 0.03215470722975334 -0.06621504620132651 -0.057202473970260556; 0.03899097797944084 -0.0541010495031209 -0.04437035069889279; 0.04467776739937306 -0.04067992873557019 -0.02923518241367051; 0.04933972022676261 -0.024386103562346783 -0.010272768238740664] %
+
+Mass Used: 1444.6973474601969 kg
+Launch C3: 196.6723576319944 km²/s²
+||V∞_in||: 2.0738863788707107 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-29T22:43:36.591/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-09T17:38:19.762
+Launch V∞: [-1.1540177007372212, 5.360837098498792, 0.2984944317979115] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-2.0043098166092546, 1.5028334917558672, 1.4743578319466457] km/s
+	V∞_out: [-0.8356117752464607, 0.15439829082406908, 2.7798876463250943] km/s
+	time of flight: 1.5586920017281148e8 seconds
+	arrival date: 2029-05-18T18:38:19.762
+	thrust profile: [0.1725379661821492 0.3028636782963449 -0.14594530225449512; 0.24010663973374377 0.25478985696879275 0.09151945430842105; 0.11381352719375167 0.3130894749849403 0.2091089750468684; 0.30283734986847677 0.21701222794179637 0.09824137709532094; 0.03630275234501889 0.41675693248956935 -0.1012386700554873; -0.2418245491826651 0.18118147964342593 0.21825116267504735; 0.2915470156543983 -0.03388072887705498 0.24410561878006867; 0.412361768542535 0.2999336398088819 -0.03160436499097794; -0.3812539424180171 0.37480489610907414 -0.03459460167463225; -0.2611116851421491 -0.2829019647433105 0.18194015849684886; 0.38117772281170925 -0.25992909797801095 0.11794074908818503; 0.47844764750593854 0.40046145886582907 -0.038809743471385535; -0.46688744880086946 0.4632135549542049 -0.04628160942646042; -0.38034093441997535 -0.3405512606021152 0.10677210042434881; 0.31086761425082576 -0.4048490143871347 0.1223843991365784; 0.563950253001912 0.04920151532400937 0.02450398411122806; 0.3683993286573054 0.6302412619336084 -0.0857920129848164; -0.5891033244964972 0.368112076435439 -0.020783964084951624; -0.43285871121985753 -0.4273820767487316 0.09610577284114862; 0.2491356450509427 -0.508230954127345 0.12331066638000482] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [5.611204987956414, 1.0148015551991953, -0.05634775428610248] km/s
+	V∞_out: [-1.1695945563190893, -1.5488819990446605, 5.3620550672788685] km/s
+	time of flight: 2.0545559999887675e8 seconds
+	arrival date: 2035-11-21T17:38:18.762
+	thrust profile: [0.5107734951887763 -0.3946064078009902 -0.0045676369422384165; 0.4598697444727305 -0.20748812220867774 0.059353622926187184; 0.33581510576782936 -0.407189511957922 0.15987153660020692; 0.3794276589018478 -0.37511266169747637 0.14960397348233373; 0.13533934017940225 -0.5031320027541039 0.08209543124670671; 0.4245206324807559 -0.6227802169786933 0.05650960675506308; 0.6558675736258086 -0.3397032003626548 0.03308794472495331; 0.5120131659823914 0.2924383586904873 0.05184380445957168; 0.34826053012663044 0.014522849649912385 0.19696263006429715; 0.041523907241033706 -0.3360187093015938 0.21706268681577065; -0.3475762260365926 -0.48685037074106274 0.1315856784159298; -0.3743319370307219 -0.6764350725170731 0.0903118551039194; 0.5097342414424403 -0.7734829334242606 0.09514159989066195; 0.7845273733985942 -0.5753935364819165 0.029842770779258728; 0.7315778039847924 0.3432605037934376 0.004749315755486527; 0.5968872158984753 0.44198729718418783 0.051253635005704054; 0.42636307680116 0.379616657506637 0.10303815501796434; 0.22195498303040814 0.27300879237608766 0.14632762929547719; -0.024188484440234567 0.13680033465416566 0.18166786525750667; -0.25695040241576644 -0.0340498293709866 0.19810666574939037] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-5.337830290816849, -1.2797414036157133, -2.7683894000988465] km/s
+	V∞_out: [-0.10980431423849103, -0.03384798680602295, 0.02827033505965302] km/s
+	time of flight: 1.8897119999873626e8 seconds
+	arrival date: 2041-11-16T21:38:17.762
+	thrust profile: [-0.18827080027303889 -0.0037944481429670707 -0.03587675027570545; -0.19565231042967327 0.005129353701615244 -0.0491082915163806; -0.20133676663900688 0.006029178811167082 -0.061481112982642354; -0.20302516058528305 0.0007224209388200189 -0.07282963982737341; -0.1992472102885178 -0.008123574893217902 -0.08261210764249102; -0.18966342972050407 -0.01766000522047062 -0.09006550432571891; -0.17498658801374278 -0.025605649979007036 -0.09448626862190662; -0.1565946658088734 -0.030702577951425794 -0.09546452816058656; -0.13601668286185079 -0.03270754112415236 -0.09297644549658375; -0.11452486200770591 -0.03205112806212533 -0.087329135163873; -0.09295108976564484 -0.029437401451120573 -0.07902523194922431; -0.07170872328897128 -0.025556470851551057 -0.06862784111694957; -0.050921087058557565 -0.02094394138963416 -0.05666105407220744; -0.030593668268616675 -0.015951410990809784 -0.04355220139864001; -0.01089690262146556 -0.010781661120095435 -0.029616221718477793; 0.007122614981337976 -0.005737608245027011 -0.015721445566949432; 0.02554588657835649 -0.0012054841338314535 -0.004144072671787097; 0.04638165061824139 0.003923812353691581 0.008511361629231926; 0.06771364374279902 0.00950332978700583 0.021885568118429555; 0.08936998361099453 0.01545954630179973 0.03535590621212607] %
+
+Mass Used: 1812.515221885309 kg
+Launch C3: 30.15943017607013 km²/s²
+||V∞_in||: 6.147694701615383 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T00:34:25.423/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-23T20:49:35.793
+Launch V∞: [-2.4450865737116274, -4.101829409199476, -0.21378743337924264] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-3.9454321781223207, -4.3349983737367435, -0.23163519766252774] km/s
+	V∞_out: [-5.484540365422154, -1.7912021635297986, -1.0612283164832435] km/s
+	time of flight: 1.3168651513492899e8 seconds
+	arrival date: 2028-06-26T00:24:50.793
+	thrust profile: [-0.120722733695335 -0.012176360827686798 -0.030518390794883023; -0.11679617667506606 0.0014999178722870938 -0.035606031789671; -0.07727822397577828 0.3037973459191278 -0.0585534522901871; -0.223884565034074 0.38469778038311786 -0.018658505423278564; -0.5047726947284132 0.1198586588428443 0.04363822566057665; -0.36008917896849646 -0.046966759269397945 -0.012020139167426613; -0.2303697349032088 -0.18990779273074385 -0.1162523931176612; -0.009059953396105604 -0.1826064551186425 -0.09566243569922224; 0.06464171493355703 0.15348717344682897 -0.03592117858719949; 0.039222535062581575 0.45251270837425567 -0.002237551646205031; -0.3129537896040898 0.5005808668195679 0.06976206030714757; -0.6334356581244346 0.342167669148952 0.08785885490233064; -0.6259891593556097 0.07036975867629339 -0.029340487056482453; -0.45498760154179435 -0.5093792240633872 -0.13924939952781157; 0.03362679051118392 -0.46176686054217253 -0.15798494014212214; 0.4358161230258788 -0.13839418528576888 -0.05039097669674436; 0.3044870713576448 0.4992315283787602 -0.0039116386904277205; 0.17193614377332783 0.7613325121786818 0.03200649181430257; -0.5572427328043519 0.7854289375339618 0.10069718693059672; -0.7044302858314516 0.6325274227780806 0.1358242855667267] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-4.177197074414225, -0.9720140804548069, 0.2337469329489975] km/s
+	V∞_out: [-1.1897818013258668, 4.123843236773216, -0.16384853893411477] km/s
+	time of flight: 1.0354715657281214e8 seconds
+	arrival date: 2031-10-07T11:30:46.793
+	thrust profile: [-0.9480754862164437 0.3056342864181156 0.04775925131934315; -0.9545036085062072 -0.08916062469268374 0.07006956877613481; -0.8556415500647792 -0.5308952023053652 0.07581953613413958; -0.6525116764830651 -0.6804771046594907 0.072044066669931; -0.4141337602665943 -0.687613497545176 0.06325121629083955; -0.2876119881822729 -0.56915707346219 0.04608924218869737; -0.23061087236806183 -0.4285889382631892 0.0353521662171739; -0.21444588630200445 -0.2987113553031206 0.00894677998389626; -0.2042602334001383 -0.19716033565885058 -0.010540546258761902; -0.19797650808153522 -0.05516030431031445 -0.02296358167357804; -0.17870024970353923 -0.051487903415797315 -0.028673002243452296; -0.16087764941466745 -0.006028156883433786 -0.029496266489663633; -0.13249691125920962 0.010594568264314964 -0.03373869555595076; -0.1023119680343583 0.024125699413220757 -0.03194152432595998; -0.06667052712715316 0.022162434908797966 -0.0413032534053769; -0.02650461479736716 0.019860230188950657 -0.02825273461209873; 0.008483997200284142 0.010514866140007597 -0.027548374980192067; 0.044674954681201196 0.010390355078242345 -0.02558959064331584; 0.0698391445723141 0.01711123350841671 -0.025534958302052144; 0.07369308900718043 0.036955143265610016 -0.01808340139735954] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-2.855151769198392, 1.832432120626587, 0.030050486577809125] km/s
+	V∞_out: [0.043566731882813375, 0.1453515199166137, 1.1921829828355344] km/s
+	time of flight: 2.616408348306797e8 seconds
+	arrival date: 2040-01-21T17:31:20.793
+	thrust profile: [0.04225281791313958 0.029025037669065452 -0.0022530954062099607; 0.03735188618997079 0.03969404585926613 -0.001990942517015921; 0.027816672613794786 0.05946905402188188 -0.0018579377168727645; 0.013243713257944257 0.07889753909094255 -0.0012755910819474462; -0.012739124713320801 0.09684893162964908 1.027454400474268e-5; -0.04822800674369958 0.09918628844749049 0.0017567047619653946; -0.07935450012796613 0.08394550684634153 0.0037636317001541555; -0.096945253591464 0.05610257601854072 0.005447062756033347; -0.09806004451336248 0.030655118745335445 0.006892840256261471; -0.09160482001962598 0.01129333668797376 0.00817823646747505; -0.08125465088354236 -0.0016801849370562216 0.00916589692955618; -0.07057826106211562 -0.012831389696222687 0.009635922957337987; -0.0608971186898785 -0.022237451930920055 0.009413611150840169; -0.04763682121829541 -0.030887917780507177 0.00991332083072347; -0.03427587291576678 -0.038223126040402684 0.0087593563060389; -0.020871167351686367 -0.042373328878652756 0.00605668309720862; -0.00993028466867035 -0.04326291873459541 0.004363203651694872; 0.0023913294032781693 -0.04518734156701757 0.0026868963953325204; 0.01211694278076428 -0.04625260852612796 0.0010932842321948841; 0.022158514510870343 -0.047555924847739336 0.0009362531581306844] %
+
+Mass Used: 988.3534236974547 kg
+Launch C3: 22.84915792178947 km²/s²
+||V∞_in||: 3.3927278307586537 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T02:33:04.261/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-05T00:35:20.996
+Launch V∞: [-3.2137533909207794, 5.084712824855146, 1.430949155734375] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-6.255155316138288, 6.606484457110347, -0.23100377774853306] km/s
+	V∞_out: [-7.465384617443416, 5.187341596386573, -0.43088705744489453] km/s
+	time of flight: 1.3257925555072227e7 seconds
+	arrival date: 2025-03-07T11:20:45.996
+	thrust profile: [-0.007759166593782 0.008081441978955738 0.004825043238403784; -0.011235947824502553 0.006629595221827023 0.005298768481147631; -0.014134476908100888 0.004950559801138478 0.006335721099905584; -0.016912120418734602 0.0032538753168045408 0.00722543103380731; -0.019615343774186608 0.0015764448870706 0.00791543407768123; -0.02224614170581595 -0.0003222442781983473 0.008542627265521198; -0.024752022364092727 -0.002502638264186997 0.009081125608978445; -0.027074692908356103 -0.0049669389909122045 0.009549338120131428; -0.02919125492967198 -0.007632280649054239 0.00984618903400726; -0.031034823850380824 -0.0105147854228823 0.010076901834442997; -0.03258867449421671 -0.013557927955447253 0.010239842439460488; -0.033896907887579285 -0.01664233072935544 0.01017836634561616; -0.034798910393570345 -0.01976899064579983 0.0104762622470642; -0.035510243080800585 -0.023010543051237668 0.010185800368979887; -0.035958245848237244 -0.026088542265344326 0.00997354827689359; -0.03616255540821458 -0.029107623361033046 0.009767283341448791; -0.03613539245186166 -0.03208125702710542 0.009490588816176345; -0.03594590447689291 -0.03485698552669035 0.009220695825097646; -0.03554558605538018 -0.037576230560006675 0.008899820851614233; -0.034817304760338785 -0.040399339549697474 0.008549184269071997] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-4.869253095327301, -1.0830259181507658, 0.41420291406622983] km/s
+	V∞_out: [0.7972771522364179, 4.941460361504594, 0.0211284831130985] km/s
+	time of flight: 1.7681537153208575e8 seconds
+	arrival date: 2030-10-13T22:43:36.996
+	thrust profile: [-0.4667533593525884 -0.39491731925461715 0.09187802488824132; -0.2763903182910042 -0.37035074693961667 0.09861113689219381; -0.16222846365284407 -0.29220875981191247 0.08972904873143848; -0.12809339133608721 -0.19599395109677922 0.06703442708591248; -0.12151618016164137 -0.04686965062834339 0.033439069587540726; -0.10811409035917058 -0.009477194232797893 -0.012143321662504066; -0.10924801926559909 0.14082268122578098 -0.05670682044948156; -0.029758444441605168 0.28004126085284164 -0.08287077095226834; -0.005277793889388453 0.43294397265469803 -0.08212135825686287; -0.32054145122009575 0.5753532885361126 -0.03968329559118082; -0.6812467539999161 0.3089367113933967 0.051808034060789085; -0.6510836214832658 -0.4873937421666415 0.12520004751950561; -0.49557588979996686 -0.512322294250635 0.15992845574394862; -0.34374129520368857 -0.5135522557199093 0.16537305271566424; -0.2240792189464561 -0.45518516492142325 0.1550538281965299; -0.13865236852037352 -0.37950308770911234 0.13394772771689303; -0.0785171269810383 -0.2978976352535766 0.10596692987800144; -0.035327531433840355 -0.21564018776939112 0.07474526871132638; -0.005605243694407901 -0.12702627457742785 0.04128648833249606; 0.01020681436565993 -0.02502132504960536 0.004261721313786419] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.9690596099587732, 3.2707822497004333, 0.03981900780395632] km/s
+	V∞_out: [5.114183571314532e-5, -0.00028059524048684205, -1.0322857139071202] km/s
+	time of flight: 2.4691764297066832e8 seconds
+	arrival date: 2038-08-10T18:57:38.996
+	thrust profile: [-0.010548481282575234 0.04258751351881362 -0.025726963732731655; -0.01128130800439453 0.05537735517283375 -0.02522998253773597; 0.009886584360292121 0.08885355612430626 -0.02421777901196621; 0.034425823426465496 0.1204073126801249 -0.020057117827333014; 0.039281760158963876 0.14271215958548816 -0.013510596261601598; 0.018736852336642556 0.15327407334940432 -0.006130067311322509; -0.022719461407261828 0.1451025891518733 0.0027035496704120453; -0.04847577536899553 0.1212275153694897 0.010891420241408132; -0.06628322085560583 0.08574069656011961 0.01754569902422787; -0.0744351565286978 0.045598034397603175 0.023036321178276163; -0.06578589050933895 0.03204645107589838 0.02550340232781789; -0.06050564660450317 0.014954861896586048 0.022962687464765534; -0.054168514931042216 -0.0014952150532753753 0.025171195023900708; -0.04623865244234472 -0.016264370557547467 0.0242622456069454; -0.036824077689454164 -0.0297205445345202 0.026079813616960393; -0.0019119020757232493 -0.03990997756665856 0.02228921048798602; 0.00955546353811231 -0.039278332497075394 0.01302479870315554; 0.023384650419100452 -0.03759767262766218 0.006978165358701964; 0.03212872391392216 -0.041380395386008566 0.002045914746881736; 0.042058274941623244 -0.040048678289472804 -0.002284527484416767] %
+
+Mass Used: 739.6059104634573 kg
+Launch C3: 38.23013085519812 km²/s²
+||V∞_in||: 3.817957284453156 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T08:40:36.355/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-11-29T10:54:51.469
+Launch V∞: [-3.0580432001025106, 2.2375690420359073, 1.0588738801940067] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-4.571073362651481, 1.5280878123442105, -0.45427388957404374] km/s
+	V∞_out: [-2.4964790697852464, 4.131812654452342, -0.3633277130442272] km/s
+	time of flight: 4.098218966605439e7 seconds
+	arrival date: 2026-03-18T18:51:20.469
+	thrust profile: [0.02250623498780786 0.056715344804171675 -0.034873620216503566; -0.01586442265299213 -0.06295338578554689 0.08519483155847359; -0.01017916810128589 -0.13656445837778508 0.13681516443703864; 0.016841859589487678 -0.20255260280181142 0.20891399350975495; 0.062143156420800975 -0.28723660826482245 0.19358888229070814; 0.12715651158662364 -0.3394613038803359 0.20147574219826075; 0.20972581667196719 -0.36860712178143235 0.1951519573601803; -0.09233171629208815 -0.37108179526235385 0.17885323373772358; 0.3963663785610897 -0.36411236763263627 0.13917684957996404; 0.4803269916210104 -0.3294208336249097 0.09820475158586775; 0.5482500580902477 -0.26964129417960103 0.048521784619223775; 0.5975936677510483 -0.19019649689789742 -0.002336850116568105; 0.6325139378587388 -0.09620606406958827 -0.051883810140986475; 0.6526011444191557 -0.033184627930530654 -0.09806508414837138; 0.6603449674456996 0.03554980785042415 -0.14075413564780873; 0.6548829138633075 0.1249977655026878 -0.17838380784227764; 0.6314304294837665 0.25982925441811655 -0.21188069709202154; 0.5851498705012528 0.4073099939525669 -0.23422861887565163; 0.5033984822411408 0.5327877791886333 -0.2470941526499058; 0.37097506574856026 0.6250076852929124 -0.25134269316042973] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-2.888718591099067, 2.98093500374621, -0.03527346962365893] km/s
+	V∞_out: [2.3790932465957977, 3.378686597227906, 0.3953591906305017] km/s
+	time of flight: 1.0806802469609727e8 seconds
+	arrival date: 2029-08-20T13:45:04.469
+	thrust profile: [-0.23488496954455496 0.9896419507072445 -0.11601157743285787; -0.948717799093386 0.9810049502433882 -0.11137913018095054; -0.9878845940359288 0.8353827321448694 -0.08704039668042218; -0.9873512008683539 0.283891063339361 -0.05113640206170415; -0.9867884331885424 0.06209683131941994 -0.023752079481471355; -0.9535019575354626 0.09042898307599517 -0.006869177979295686; -0.8629780107614938 0.07500054807185184 0.004358596231624515; -0.7266566061890536 0.04691475374478784 0.014062645283394093; -0.5808329590842135 0.03171216226293981 0.01492806895495031; -0.45651135691182687 0.02498400153146004 0.02067482320548018; -0.35501493081559393 0.019422083647277044 0.02044779215749133; -0.27657576243518855 0.011215381224156324 0.02020194799272021; -0.21016915317145918 0.0012589829531977736 0.018128327930858827; -0.1540086140112979 -0.00846566443167276 0.014833095420263493; -0.11001947393418925 -0.017257120988655155 0.010078742680114872; -0.08042976828632163 -0.026027288334698796 0.0033185622120666994; -0.0629225614505061 -0.03930242635942339 -0.00425731557389946; -0.039084131760545315 -0.04757303261125456 -0.007171372481770967; -0.02892366311071207 -0.04758562095515022 -0.027423761082656064; -0.032231185187749124 -0.05078891683404573 -0.03274525516746696] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.031508320728017, 3.034062901615318, 0.15878852483474554] km/s
+	V∞_out: [0.2528673092202353, -0.0017020120539992514, -3.464904646047938] km/s
+	time of flight: 2.8592742241253144e8 seconds
+	arrival date: 2038-09-11T22:02:06.469
+	thrust profile: [0.061035494563444134 0.11929805743419754 -0.05461112133488575; 0.031266058641029826 0.10685642176058087 -0.06293750177877995; 0.027970653885991688 0.09862792518563299 -0.045534907819447135; 0.04107581844710626 0.09322334760151729 -0.04122709275105615; 0.028048942877953027 0.07458987618035917 -0.0293725553620492; 0.024315747642101215 0.10122639432961994 -0.018308088524984865; -0.020351662679905323 0.12588983468280268 -0.003296359905923822; -0.07496938768838549 0.13064499952764547 0.02049090758833104; -0.11466260045345358 0.10481780256514156 0.04012703743869543; -0.13862140670508313 0.07032047401299907 0.05293678290006058; -0.12563192616320198 0.03543281578759781 0.05260279035660168; -0.10942634615118742 0.010406138047878839 0.04847794436412976; -0.0883793299482217 -0.005946135827960692 0.04035916568664598; -0.06302255227760427 -0.014764403237537608 0.02898877705275781; -0.04498980023607455 -0.018979702934655323 0.018607571396221836; -0.04140068077722925 -0.021838625953655242 0.012261185161105725; -0.012314656602333676 -0.007156039336999209 -0.0015716845681593603; -0.010603730130079583 -0.0013797109292671373 -0.006338804956808768; -0.017028324565081396 -0.005918175097290475 -0.004776176869816615; -0.020105440868362738 -0.009689084862531186 -0.0020482929935368567] %
+
+Mass Used: 847.3804986047398 kg
+Launch C3: 15.479557325727804 km²/s²
+||V∞_in||: 3.2085449821233127 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T13:52:11.363/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-15T22:51:31.653
+Launch V∞: [1.0265298829626757, -6.097752351134353, 0.6856608803521997] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.685353880716249, -3.6396637778190533, -3.2013166230561305] km/s
+	V∞_out: [0.5302103364593528, -0.9765757196202859, -4.767844807662866] km/s
+	time of flight: 9.971640000084461e7 seconds
+	arrival date: 2028-02-13T01:51:31.653
+	thrust profile: [0.13284751649644205 0.9411989426214641 -0.46977683989334873; -0.968547907767294 0.9608251103851381 0.49339267132424175; -0.9787154450158303 -0.8432228864566057 -0.5543030062336614; -0.9458849725429278 -0.9442327236046363 -0.7636886633819076; -0.9667535016847152 -0.7358061408218618 -0.11636279319023346; -0.9820303864106136 0.7930475060706941 0.4962497106503541; -0.971227150319471 -0.986463218458502 0.4632222480421968; -0.9271319319791395 -0.8917240929018778 -0.6101593732712101; -0.9139137651217345 -0.5324029885065178 -0.8083289582144534; -0.9773913889808017 0.991657638900593 -0.4106474876750948; -0.990512335176245 0.7321537085435096 0.6605421761973608; -0.9581179828820583 -0.984882219664571 0.6421847460531694; 0.9803502761290055 -0.9432783942684786 -0.7125092685705092; 0.584101463120002 0.9947933997204838 -0.8808317684328829; -0.993526887524295 0.9941311908456837 -0.7387372801949493; -0.9957384470386984 0.9741994738088207 0.5708597976999408; -0.9915748324180956 -0.9960584321805054 0.8295257560724948; 0.9959387668352474 -0.9942746434271464 0.1695440717133519; 0.9960944736420316 0.8745766502055389 -0.7915289853600778; 0.9903811167032217 0.9961817491550279 -0.9573032378642442] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [2.090864620573387, -3.222147331578074, -2.509087132015622] km/s
+	V∞_out: [-4.488106073949989, -0.5175537490206633, 0.7987014856646427] km/s
+	time of flight: 1.6423199999993336e8 seconds
+	arrival date: 2033-04-27T21:51:30.653
+	thrust profile: [-0.5660855310698739 0.9967906693759188 -0.8209919327744069; -0.994170631248832 0.9947713712108747 0.1448631429571182; -0.9945000494219841 0.9274125399233997 0.4897574376167066; -0.9894742986247569 -0.4507820161619902 0.4166941133651491; -0.9714202588117182 -0.7137518679961032 0.30094666125802183; -0.9405225764860856 -0.7041104481825169 0.1892804023301685; -0.8322614400348775 -0.6078444193505477 0.10175874680514145; -0.5733990958821588 -0.4496883690491375 0.04286046670382909; -0.2872975060978055 -0.27194044695575137 0.01185750904851918; -0.03409685881889757 -0.09226785043335413 0.0007765631982848799; 0.041566915656923824 -0.02743199843891902 0.0012223583050356183; 0.03704247583337095 0.003644238002607764 -0.0017388167642256004; 0.055997436147982374 -0.022254514712059217 -0.007208925051407416; 0.24811520314082097 -0.1362846587264196 -0.02883669922015275; 0.4207497452192147 -0.19686359679762824 -0.03935341240442315; 0.5330387060152292 -0.22897802946531448 -0.04350654265126503; 0.6138159398623063 -0.27334600431296685 -0.042974346394558584; 0.7031513931411775 -0.3631789642405433 -0.03783836908358169; 0.8144978524655395 -0.5249342706264041 -0.03246396629051213; 0.8897103992638571 -0.708341160251077 -0.03341117930579575] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-9.950524772292589, 2.7136858826882397, 0.8437847433534009] km/s
+	V∞_out: [-3.9746513384546427, 3.419068378994426, -0.22492206192340505] km/s
+	time of flight: 2.4062400000004002e8 seconds
+	arrival date: 2040-12-11T21:51:30.653
+	thrust profile: [-0.026861539030662098 0.053037742486198663 -0.03998103891716118; -0.4005257165378705 0.12385064839383274 0.04228749257228828; 0.11316689356297174 -0.5002033317813458 0.0920099903831136; -0.4310529749448192 -0.3737769540652961 -0.16434453658789766; 0.524935339397772 0.326736433374278 -0.011049835879189725; 0.2870548648523757 0.9008250510979924 0.043684490460944636; -0.2578688762031856 0.6811275515417524 0.06979705435650777; -0.16643689458434993 0.44448647933073615 0.03748178826678883; 0.03135747943986613 0.09121026982102139 -0.011021906895529003; 0.2773784563100772 0.21421663651317946 -0.0939720012037749; -0.026321949219467622 -0.002583681933706951 0.0022197546795018445; 0.20252009126605577 0.5859029556414175 -0.10288257122681152; -0.5835246166241774 0.9904709316092567 0.042044833954454276; -0.7362038421319124 -0.20746802611665538 0.26205247161144074; 0.025644898980856885 0.13288887758204784 0.067531572098157; -0.1567362766945195 0.020710809244175152 -0.029197896508943184; -0.35499348849403123 0.09675115246414323 0.0008648920068945578; 0.08552766541451494 0.35786531030916835 -0.019970820204502436; 0.07564615169332112 -0.16796111456618562 -0.022460352690263453; 0.25493279832576426 0.09735303708739874 0.0929229928187175] %
+
+Mass Used: 3003.684776260021 kg
+Launch C3: 38.70647817922525 km²/s²
+||V∞_in||: 10.348381854523241 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T14:09:25.262/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-11-16T09:01:46.766
+Launch V∞: [-1.2358227541627522, 0.323049558821953, 2.495135844447432] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-5.492217326783208, -0.7599139192265875, -0.7445133837270346] km/s
+	V∞_out: [-4.404936994877108, -3.4463054890902294, 0.12597397946441688] km/s
+	time of flight: 1.1637720070766585e8 seconds
+	arrival date: 2027-07-25T08:01:46.766
+	thrust profile: [0.01055136636996065 0.5035473835223019 0.2144643592551079; -0.04595477215059715 0.6852423614947899 0.16820399057019442; -0.5895802429453626 0.7197253917092584 0.15157285154237687; -0.7242691347954416 0.6365969821781644 0.18351832934110204; -0.7254557218972608 0.33325583626785743 0.20650030599325478; -0.624534757383007 -0.46380253719846265 0.19914261964212518; 0.06888536686167775 -0.3659727992321626 -0.05660421386154573; 0.41960359345145115 0.5802522947366238 -0.02564875636361316; -0.43557904354293114 0.6848106459808407 0.15045741326417394; -0.5906326245605844 0.626327253137284 0.1907051751516841; -0.6145984992977067 0.6853285910994333 0.24790988830917382; -0.7852172198133732 0.397363217233713 0.22913677229660695; -0.6148113166692493 -0.6180162700085184 -0.1063370011071445; -0.3438743055901661 0.08561279547696703 0.1133320954927072; 0.24423988113626285 0.4984911769229264 0.26361771766972686; 0.6070536708822735 0.7233947175576885 0.2890649522953669; -0.39805774605395056 0.8544543105302159 0.2032769540887175; -0.877234342411992 0.5568182222065088 0.1181949174776601; -0.7848468400087453 -0.7818849886318364 -0.025654657156075657; 0.39491632368805846 -0.7677648336006526 -0.018827493121373502] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-2.011375822763062, -4.005960504046318, 0.6209700805836994] km/s
+	V∞_out: [-4.246987681230396, 0.16498798356943736, 1.5540119004205253] km/s
+	time of flight: 1.4691600181840378e8 seconds
+	arrival date: 2032-03-20T18:01:47.766
+	thrust profile: [0.681909870255602 -0.5761969653838755 -0.02754846539663112; 0.7118573450786314 0.31247951434638493 0.043677226876746314; 0.5476987320075556 0.6581866365943503 -0.003833400581880826; 0.10725439389134384 0.7294932911664623 -0.034290527364056536; -0.5427655230030919 0.7281280491625349 -0.0299219686998862; -0.7331645357201648 0.661529122002647 -0.022598124369638494; -0.7921492428190279 0.3933778983017051 -0.021082156107776216; -0.7932731599235451 -0.41313404927011227 -0.019757316586946027; -0.7424285866522327 -0.6896359802485261 -0.021540954373280186; -0.6106751913915949 -0.7225982342788454 -0.020163701822483136; -0.37316409906634423 -0.7007771556440968 -0.011208908465949893; -0.1711206238316838 -0.6415857635215466 0.0059500126042923785; -0.08270331405821842 -0.5687506908923067 0.02659262994655598; -0.049372522261264505 -0.49783910816632987 0.048628191706214005; -0.04372663474025917 -0.41699938093001865 0.07363018971956578; -0.05490501770449129 -0.31189423172940106 0.0949294276017952; -0.09260972837599633 -0.2199470543952063 0.05957362145438097; -0.0634254159444419 -0.17400774633467572 0.16341908215231168; -0.05232699030024355 0.08812711882068765 0.1012502462026133; -0.04359653224713776 0.2114603900012656 0.04944539701697088] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-7.936261563870153, 0.192812008719828, 0.7850203435347649] km/s
+	V∞_out: [0.08172234404293398, -0.35122508987936396, 0.006338068922481654] km/s
+	time of flight: 2.9010960004261374e8 seconds
+	arrival date: 2041-05-30T12:01:47.766
+	thrust profile: [-0.1762427833398218 0.018451914856523026 -0.33296833868061293; -0.10855107710674605 0.044463310211183146 -0.33965829997250213; -0.04955955263781527 0.10666486336804054 -0.3343168817737069; -0.14933152742910255 0.1645563456813175 -0.2888802750452695; -0.011372547689235173 -0.39964858425741717 0.1289083844812905; 0.17913823101853307 0.33922366300742973 0.3624022918784145; -0.056147608885838356 0.40536943517001855 0.2345805092442894; -0.11646645449972745 0.37970664664911913 0.13215537014712256; -0.10774775336158972 0.3637144687183163 0.07982907905717164; -0.03689877185389765 0.36730516793108037 0.04229495484147119; 0.08041474785484633 0.3975271403801768 0.011450007794323156; 0.2209067582381832 0.4645747308847809 -0.016359218295681436; 0.29077903309671577 0.5746646081920227 -0.03785392741655643; -0.5440697079277356 0.7004154769551414 -0.02197571950265878; -0.5081898184366466 0.06445088273594297 0.0502311733117999; -0.19802320496526152 -0.07027856584170135 0.014625860167883831; -0.07715652979513347 -0.015846719041313496 0.0076264391612288025; 0.180938962168102 -0.0850580439905663 -0.026509928911235665; 0.28645290190644923 -0.11681132361576753 -0.037935422919142044; 0.4089515815441177 -0.14951729956288723 -0.05914131349793209] %
+
+Mass Used: 2473.604423137509 kg
+Launch C3: 7.857321779407867 km²/s²
+||V∞_in||: 7.977322923176217 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T15:47:59.016/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-22T06:44:51.639
+Launch V∞: [2.575248384952663, 2.739716813210934, -0.38893905027836745] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [4.32111461530485, 2.7960291205842593, -0.489556914131019] km/s
+	V∞_out: [1.7907908980924474, 4.820115223157361, -0.5379099033537726] km/s
+	time of flight: 6.124238397428751e7 seconds
+	arrival date: 2026-07-01T02:31:14.639
+	thrust profile: [0.02204617368488705 0.06285779065282272 0.012605171575819224; -0.011433803484298078 0.08848061166582002 0.07202092139015609; -0.07959321828350713 0.11796051271483557 0.10864894932433573; -0.16842886185138436 0.10168512037796995 0.12068506836380218; -0.23809792134546726 0.03408694703096996 0.10782537552663919; -0.2712846099916887 -0.05259050616229293 0.07714680434548718; -0.2691701026056171 -0.13114175093946576 0.03494697732427611; -0.2432473375546796 -0.19827411241093662 -0.012549713355480184; -0.19688682555894857 -0.25454624209774884 -0.060002522712937; -0.13420719992703317 -0.31198661132994665 -0.10268341121799718; -0.01782601669889528 -0.3411050774098038 -0.13846230630135042; 0.17407803978077827 -0.3653166442745793 -0.1617162480750069; 0.39405333004023496 -0.35863769585862276 -0.16764222379359453; 0.5881727003228676 -0.2918230276130316 -0.1538361990366852; 0.7349673257433222 -0.12576056403661834 -0.12169301624150872; 0.8068721878811431 0.08212623367867798 -0.06681093685570723; 0.7498334641941427 0.6273302531285769 0.0041442783835015165; 0.48778675631358515 0.768425653968566 0.07684034445879483; 0.03235026516840393 0.7961138086551178 0.1340769950940127; -0.187175909543306 0.725754663622694 0.16344645357600582] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-2.776889048582584, 0.577121588676522, 0.007961135089457616] km/s
+	V∞_out: [0.7615534564462777, 2.718708568232091, 0.27004925013867337] km/s
+	time of flight: 1.1292109290692344e8 seconds
+	arrival date: 2030-01-28T01:29:26.639
+	thrust profile: [-0.840176369612668 0.976860342718164 0.058196195949256124; -0.8628465472635846 0.7633342124306659 0.1067403299239058; -0.8382024712014463 0.2581297893476549 0.12338258921323142; -0.8025794731065865 -0.1952513411331264 0.12149932865338556; -0.7572209152982607 -0.32000638227817424 0.10891070865997188; -0.7036267077800332 -0.3720841081186767 0.09043232925350977; -0.6463345866299025 -0.4293290426371054 0.06661829901893401; -0.5816014177883754 -0.44981649190131995 0.05067422918383243; -0.47351459443415633 -0.43975356881090427 0.028888383104343048; -0.4446429769285578 -0.4496298163012175 0.016442900362289542; -0.3753382613887226 -0.44043470262281187 0.004400618346128699; -0.3104508002843935 -0.4100796118163795 -0.004420648978465791; -0.2535633130657495 -0.3762527335843237 -0.010222789989029061; -0.12727676625203097 -0.3385883342435648 -0.016879911592349858; -0.17160701300131967 -0.303175547483604 -0.013946042678809141; -0.14486147929059093 -0.25597770208827797 -0.012578650709578849; -0.12478337244188682 -0.2047807012949446 -0.008914893875013217; -0.10754382990114088 -0.15281428358709293 -0.0036295313604368246; -0.08430003348112626 -0.09766774422527713 0.003387978072041825; -0.049542730705205464 -0.025733639517012987 0.003344362241873508] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.4245259099537633, 1.4291602238263075, 0.11854473850651923] km/s
+	V∞_out: [-0.6879338015175315, -1.3876319593718838, 0.8808502953774751] km/s
+	time of flight: 3.408146015783399e8 seconds
+	arrival date: 2040-11-15T16:12:47.639
+	thrust profile: [0.0209250957876161 0.07236548568951691 -0.05441358281175795; 0.04271088201266738 0.059837108824994496 -0.04570267674006564; 0.06660112060615696 0.05195757710585663 -0.03370174018627228; 0.07859207469254972 0.05915284312855131 -0.01995033274559411; 0.05470694198510173 0.07831313755730426 -0.010342114841936848; -0.01348106574647589 0.11277794394272658 -0.0034013433219311725; -0.09145707370229726 0.10312222608201255 0.005576461043330823; -0.12850299192302284 0.05752290823836534 0.01577381261339529; -0.13477884086307976 0.013206245882351258 0.018396651241394796; -0.12124443428533518 -0.016003517409004134 0.02309161441900346; -0.10385877836751767 -0.034262782555751645 0.026881849627747586; -0.08713710038230636 -0.04462790000575737 0.02664100559569609; -0.071851222306589 -0.051275998799280825 0.02033038048400631; -0.05351516590047124 -0.05503941535681956 0.024892443243640875; -0.042179454832756653 -0.05447471988772444 0.02020467463443017; -0.03024017392297153 -0.05390626764438977 0.014150662481409669; -0.01972175537440891 -0.05302868663746655 0.005230379873849089; -0.012681981493559499 -0.05225628051430802 -0.0024339834268425693; -0.0044941899601042504 -0.05698931635146416 -0.007176158051852003; 0.009984513981692316 -0.06168319332065979 -0.016333699861465947] %
+
+Mass Used: 1015.034880811023 kg
+Launch C3: 14.289226045623414 km²/s²
+||V∞_in||: 2.021342590587859 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-11-30T16:38:03.240/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-12-14T15:10:10.657
+Launch V∞: [-5.324790803109733, -2.6773113758857146, 0.3590879071328112] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-7.8280744026110485, -4.482906734167364, -0.5270128091140733] km/s
+	V∞_out: [-8.714629007362692, -2.3006682785347587, -0.6459280917863456] km/s
+	time of flight: 1.4074379597755253e8 seconds
+	arrival date: 2028-05-30T14:40:05.657
+	thrust profile: [-0.09620569960732477 -0.09890174838841997 -0.006304928381722739; 0.01019673300605273 -0.15089658441406675 -0.0021554349727457207; 0.07822408798843489 -0.11071926046790218 0.004988054677396156; 0.09762767912264393 -0.058415019885606094 0.010174486469221193; 0.09596476555630318 -0.005224025746863998 0.004950216517465728; 0.08806191952377797 0.049822770611354 -0.0010597096470122361; 0.052574331589681 0.12454094146924233 0.015095231992096524; -0.04001716917664013 0.21428169922925022 0.018454940281947503; -0.19982535032247195 0.251124726671319 0.015258419491383634; -0.42902456010053436 0.03773585135440942 0.01861953896594965; -0.2620621821264161 -0.3783347111418361 0.004523163861194378; 0.05160537420225073 -0.3786420625260984 -0.011042008482375406; 0.20360488108938318 -0.27582667506971054 -0.012821162414732887; 0.2561047977346709 -0.14853261531425635 -0.005634983638021486; 0.260486703242627 -0.01792491318881055 0.0011583161900218508; 0.23894329094312064 0.10878274252152975 0.0042064519174942515; 0.19707710072889273 0.2344075946499166 0.011104691405835861; 0.13172705128797849 0.35645392804648396 0.01747201373387731; -0.03343397706399435 0.37057486224934993 0.01628713138328902; -0.3349092116148668 0.40830706963065616 0.015783429576975126] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-5.164409827607087, -2.4015213190761244, 0.3886272138412419] km/s
+	V∞_out: [-0.10084295997962195, 5.705933697922466, -0.1469580047293293] km/s
+	time of flight: 8.148046230775028e7 seconds
+	arrival date: 2030-12-29T16:07:47.657
+	thrust profile: [-0.4843312801347405 0.17832592220013307 0.006256115010001196; -0.5117377393427821 -0.03515133875253644 0.01594069776607602; -0.4802829543105851 -0.22759690897497922 0.023218676108680135; -0.41688069406794315 -0.3255769239533844 0.02846987059703982; -0.3518609568473908 -0.3513841428236102 0.03707709560472825; -0.28197549119514226 -0.35416420109695057 0.04330975091368633; -0.22056035580872335 -0.34012444589770013 0.048672605940703245; -0.17030162641170815 -0.3176042986233552 0.054624244098160656; -0.12962198776772624 -0.29003617152610467 0.0600491991040185; -0.09552548126143237 -0.25742381683081617 0.06663476650221734; -0.06576162258943327 -0.22042535210328865 0.07376790136845905; -0.03794666493372705 -0.18080040001875886 0.07922467457462902; -0.017587190801326653 -0.144409275958737 0.07885131961718507; -0.0005846137879528368 -0.11383597257615993 0.06598144523941014; 0.012437749223779474 -0.08192500429520043 0.050363659542438856; 0.025006348976223614 -0.05271986038900855 0.03688810130605497; 0.03735035082457269 -0.023245071824888237 0.025225516789865676; 0.048771155783688964 0.00930403641764618 0.015175514053442753; 0.056121259671254586 0.03626182021235461 0.007719603871138727; 0.06549848774435021 0.06199167605994548 0.0029712452019925654] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-2.4750372046001954, 4.13041506892929, -0.09291157556920056] km/s
+	V∞_out: [-0.9590001742156767, 0.00014166531615410308, -0.00017399656356734708] km/s
+	time of flight: 2.204227460822756e8 seconds
+	arrival date: 2037-12-23T20:40:13.657
+	thrust profile: [0.1749523615814178 0.02337696203170268 -0.007290082696294586; 0.17710130749974723 0.04583257449906523 -0.00719233870000948; 0.174350248316964 0.07510311268410168 -0.00750473770426303; 0.16444589553075314 0.10998364297019214 -0.007106342278531456; 0.1384257291897476 0.1488418684122407 -0.006173412802780041; 0.08428653747267639 0.1721787470978516 -0.003985402948896598; 0.019687460364805707 0.15515729051991808 -0.0013753294272070818; -0.021656527704037976 0.12042770713394904 0.0001864640450765926; -0.039588280724834786 0.09367324460087394 0.0010034140790897994; -0.04673002735050872 0.07208768567973076 0.0013797248342607789; -0.04399767552371756 0.05335024899625606 0.0015132659877072718; -0.04235029705061875 0.03689185722542479 0.001509047848856101; -0.037623976049185055 0.022006890975873494 0.0010667085694236217; -0.031346917825053985 0.00585591622491494 0.00023425066193087632; -0.0193407989640302 -0.012237196189479828 -0.0032635963200177364; -0.011688504812844338 0.004985875856387392 -0.0034950987669932717; -0.013753919383294908 -0.020294143888963282 0.0018680092927586343; -0.0042296107469379065 -0.03029078043837534 0.002437090971995948; 0.010887719248873684 -0.04459982317696947 0.003041721188427454; 0.02500057674047783 -0.052736469222675816 0.0029604218341606117] %
+
+Mass Used: 662.0977457761205 kg
+Launch C3: 35.650337425378076 km²/s²
+||V∞_in||: 4.816094929158691 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJS_2021-12-01T15:04:58.660/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-11-08T18:47:22.305
+Launch V∞: [-4.451427517503081, 4.380713257243984, 0.9509666906856978] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-7.503625705871378, 2.9922534516224317, 0.3970744313528344] km/s
+	V∞_out: [-6.203985495450952, 5.1853077278089845, 0.19685948210225732] km/s
+	time of flight: 7.692258675246356e7 seconds
+	arrival date: 2026-04-17T02:10:28.305
+	thrust profile: [-0.05747333201815444 0.01458857211306159 0.01661972438571343; -0.07640520733942768 -0.0880498378588422 0.009291396823580423; -0.0642351947881695 -0.14583843433809482 -0.01174256444385774; -0.03591836428259514 -0.19097919421877213 -0.030455634296288725; 0.0014696729268849598 -0.21419745388390338 -0.046332000137257384; 0.043321837437152184 -0.23281386608467833 -0.057269006919827066; 0.08487576000339314 -0.23180733654869165 -0.06400789992534636; 0.12836076596832638 -0.2345880635860211 -0.06663468113711396; 0.16914897842720558 -0.2202670166100522 -0.06608715415000553; 0.20331848204335912 -0.19904198276368773 -0.06263191481516477; 0.23625994800571543 -0.18017227778817843 -0.057302223507679384; 0.26476916718248283 -0.15037417766839517 -0.05026099494873699; 0.28150073209231896 -0.11974625587737671 -0.04226763198923683; 0.2911151952723726 -0.08935809631597122 -0.032922957893997004; 0.29662192049119385 -0.05630987736862665 -0.023018382921682446; 0.3163317621362404 -0.01253021176722935 -0.013235490847343547; 0.25582892879782015 0.03994726547045516 -0.0012262871620623078; 0.20630604157449897 0.09278869993819255 0.011047803244751797; 0.13239326442164706 0.18510472327622382 0.022309378373958296; 0.0678407381537921 0.24416553319280734 0.027187329287448894] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-2.4066983016171593, 3.60782547580802, -0.0729666504902062] km/s
+	V∞_out: [2.378938038105792, 3.622859356538288, -0.17162450321036135] km/s
+	time of flight: 1.0365627669349712e8 seconds
+	arrival date: 2029-07-29T19:35:04.305
+	thrust profile: [-0.08661540144522925 0.5452498417652726 0.01940681405322532; -0.3026836754787113 0.3296518390803253 0.005983402538334351; -0.3406876005629003 0.11833095428025397 0.003356530625833691; -0.2835305485605863 0.05826412825528092 0.02255167620704516; -0.2312925636505238 0.037264277244941184 0.05388961098566991; -0.18711959340793846 0.02248626525242582 0.07873824296078222; -0.1586634246283703 0.009933258699574466 0.0871013968397894; -0.13480225405151802 -0.0016459373751799647 0.08376814481354339; -0.11717491300808694 -0.011644771387652143 0.06591943652720958; -0.12385446642299068 -0.021486105366059834 0.04559099694744897; -0.09388047865743618 -0.028093190404018073 0.021912607207877112; -0.08329274681397837 -0.03442999409177474 0.004671009919336775; -0.074293683492257 -0.039542791582250804 -0.005853738709231158; -0.06633940754759032 -0.044531789384190786 -0.009552210711090501; -0.05819808497253237 -0.047725452096228235 -0.008621886584541672; -0.052136936558275115 -0.0524395749605876 -0.002738982045574738; -0.04346694186008132 -0.0559411143833451 0.005899905372803087; -0.019037945479989642 -0.06356156997525016 0.022900432372144015; 0.03382392128782208 -0.03750155602427737 -0.01509909397132852; 0.0372737888254289 -0.03393228709124474 -0.008856011117644847] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.348151617130741, 3.372644961627469, -0.15974064227398158] km/s
+	V∞_out: [0.5003596890905858, 0.5035022711921476, 0.4902757482488732] km/s
+	time of flight: 2.6430663321089447e8 seconds
+	arrival date: 2037-12-13T22:05:37.305
+	thrust profile: [0.09042797681998876 0.08185621600988492 -0.005657240382538273; 0.08801730768503421 0.06654785786786777 -0.005370519173262853; 0.08823193892876004 0.06301303625131692 -0.005301669247083464; 0.09786240449059495 0.0767776838916466 -0.005515040644430515; 0.08471215842112331 0.09323975234752191 -0.004395184816667355; 0.06296777251631458 0.13453925938779707 -0.0025772294050847586; -0.0014186632217062752 0.15454606073890062 0.000798883942976955; -0.06382656189096726 0.14369239243391718 0.004139373253375935; -0.09924285361658083 0.11731937511826053 0.006398669227156636; -0.11580556499542272 0.09241219909488727 0.007641311131976814; -0.12704630471212713 0.0755704468000314 0.008542821687616114; -0.13059068423655953 0.05648447252052886 0.008518267583078705; -0.1375065378923194 0.029657327876499343 0.007947474105719379; -0.12731258715678567 -0.013661649213132244 0.005928368352642089; -0.08615459629776862 -0.051365993070702234 0.003434419522338479; -0.06064751058410859 -0.050519207115431015 0.004480131985829094; -0.004983547686528498 -0.05050727346302307 0.028470779024005587; -0.029138511656783765 -0.04657877128192993 0.022486478212922927; -0.035824958961586245 -0.02656318094078993 -0.022032681036760468; -0.042164309076524915 -0.03952915140222731 -0.007355989451236212] %
+
+Mass Used: 537.3508733080857 kg
+Launch C3: 39.91019323257055 km²/s²
+||V∞_in||: 3.6356242782715444 km/s
@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EMMJS_2021-12-03T11:37:09.379/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-02-26T04:10:12.359
+Launch V∞: [-4.841701064906604, 3.475969740428134, -4.8994214190507] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [0.02729198924983877, 5.017291114045934, -2.960466892478738] km/s
+	V∞_out: [-0.7796648643413417, 5.029374064409783, -2.8347788324016983] km/s
+	time of flight: 1.9570320002726743e8 seconds
+	arrival date: 2029-05-10T06:10:12.359
+	thrust profile: [0.51200489277245 0.1491712750305638 -0.5617898782756465; 0.5985472817937932 0.4314745458970473 -0.29088252333102027; -0.45166509877363964 0.5194585980906682 0.5146294788199312; 0.390520290781806 -0.5192326236428068 0.4429840782407487; 0.5160025656800347 0.43684584169735574 -0.4960808446595455; 0.5098504634472127 0.5199893315046626 0.4441400784392527; -0.49987113488322754 -0.47893620910952606 0.48036085120848565; 0.5368410355569405 0.5166822047764457 -0.4858670271400151; 0.44238316289905827 0.547824927494726 -0.4656337244770621; 0.21668892035180595 0.6021857778661118 -0.19651661385197258; 0.4341377302277037 -0.16678624993961083 0.5761938702855823; 0.5718885908183827 0.5536579188076003 0.33795675555520704; -0.39527664332753926 0.5814857962643089 -0.4679595952307845; -0.008428218148373924 0.5415048084721836 -0.45110046854424596; 0.33161932673220734 -0.45295582817342434 0.46836263037592774; 0.5280374896116378 0.5764518977818923 0.3342129870989262; 0.3107502688966615 0.5511548090736831 -0.5014473758638118; 0.07343276836897304 0.6646323168301356 -0.33765386861899715; -0.5980335383406491 -0.5746723266973839 0.15575901290142588; 0.590900565213738 0.39693261331727714 0.20472515338144043] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [3.0241033936172084, 1.6385004369573686, -5.605711794771172] km/s
+	V∞_out: [2.4283811769402535, -1.1475844477691648, -6.003401620464895] km/s
+	time of flight: 1.1737080029703692e8 seconds
+	arrival date: 2033-01-27T17:10:12.359
+	thrust profile: [-0.1768137656168143 0.3393511738335891 -0.353565456723947; -0.15954083659688176 -0.5487799730055659 -0.24022806443793981; 0.5157742145013325 -0.7252600963065111 -0.4938126290082077; 0.698500596084941 0.03900690309877106 -0.23316637699244064; 0.6365913895344839 0.20777317872832707 -0.2830962364627441; 0.5861304271928349 -0.1184358449845895 -0.4564142893293172; 0.6860855423630463 -0.5456724995449903 -0.44617293698271493; 0.6670491113213445 -0.38498567211274926 -0.3230834818585812; 0.5283999818464645 -0.09570871485046831 -0.478027472175741; 0.6580560949600205 0.46722570225829474 -0.11535896533777851; 0.5612619202113102 -0.1931961652510376 -0.4400901944952552; 0.4590177925799 -0.6932770941014383 -0.5144556676853405; 0.7561006651195121 -0.6660301702898956 -0.558073578122206; 0.7758630959701225 -0.08472708630272804 -0.41036611726373284; 0.566096622638857 0.7122289950338151 -0.11214847640185667; -0.4306590268194921 0.4288485227605312 0.2105331105689206; -0.5085374829983493 -0.516980326040015 0.16675646570585556; -0.5812762098132924 -0.6592114464112737 -0.39525785227607435; 0.3559795650447502 -0.8283244516408661 -0.5816275654619777; 0.7220122543976706 -0.8709955103801817 -0.5752271662039113] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [5.060776761478531, -2.65457156740014, 1.2093916749224973] km/s
+	V∞_out: [-4.655218918764466, -2.2507227956970843, 2.7173192390054806] km/s
+	time of flight: 7.437600000965603e7 seconds
+	arrival date: 2035-06-07T13:10:12.359
+	thrust profile: [0.5554028628906259 -0.8562653819570508 -0.4353192179666242; 0.6836770270628973 -0.8068634065800825 -0.40691024348661053; 0.6938434264699962 -0.7253280301253697 -0.3838170511550203; 0.645874750163326 -0.6289501430894447 -0.3499668164482744; 0.5889993418389312 -0.5421974665324047 -0.3250231983004846; 0.521131977446493 -0.4767106284566455 -0.3139270110389849; 0.44907608028844187 -0.42835191134595757 -0.30427273241100156; 0.3771619836123307 -0.38593020022499613 -0.29345181442595814; 0.30758537653438345 -0.34138417397604953 -0.2806050625679753; 0.24090511199415704 -0.2908278788914028 -0.2653604699658747; 0.17676587080788508 -0.23266346298480622 -0.24755096472050972; 0.11564885705822119 -0.16792372723278565 -0.22685867498381254; 0.07637432600785862 -0.10221693792171678 -0.20194486428807676; 0.019753903444897154 -0.058193667702053815 -0.18756658332981802; -0.044040327145306354 -0.00021057373845115093 -0.15565868544825787; -0.1020149066984689 0.047297427488451 -0.11989375229021738; -0.15572852811033114 0.08561531859322227 -0.08266441800646043; -0.20039007901031922 0.11872106917143616 -0.04576729741807346; -0.24124782668690306 0.1511930898415435 -0.009960538806793113; -0.28349017928188214 0.1924753920006318 0.02615368339855036] %
+Phase 4:
+	Planet: Saturn
+	V∞_in: [-7.256385977948657, 0.7771719462797614, -0.785892915072424] km/s
+	V∞_out: [-5.9473393974944736e-6, -7.362203906933263e-7, 6.306068555232033e-7] km/s
+	time of flight: 1.4662439997163886e8 seconds
+	arrival date: 2040-01-29T14:10:11.359
+	thrust profile: [-0.18959418256753224 0.13412715420236315 -0.043410183532822624; -0.19766571870169566 0.1372601657158578 -0.037968113030145044; -0.1971783405485536 0.129832118307628 -0.04157452597322259; -0.19192072677853972 0.11752160892327206 -0.04544882251204915; -0.18096355607909057 0.10099613325234727 -0.04845756455495175; -0.16440940142977603 0.0827695902679096 -0.0501168011338542; -0.14159683191947461 0.06939209018313232 -0.04938123378650775; -0.11494734465063888 0.05950353242028259 -0.04787565574075916; -0.08842871021960914 0.05331851047785903 -0.04243441932918664; -0.06244946835797671 0.049895056937498274 -0.03534701683264976; -0.0380028875571515 0.047256901837732644 -0.02725064975669285; -0.01886788294008128 0.04286456425792469 -0.019192970894846496; 0.0054749884299889135 0.041277048472854974 -0.010750429199969911; 0.02389959629376803 0.03888123568193434 -0.0015386535754099552; 0.0428231915186611 0.03753775483224003 0.00740487148339779; 0.06481451674589596 0.03713565978563092 0.014580239918154077; 0.09005525246175461 0.0369062161152353 0.018428292697994248; 0.1201760127678751 0.03212421201511818 0.04118543343400019; 0.15404590862831494 0.02789044310966664 0.043771491647338116; 0.18466591121075765 0.02447914444489793 0.052012952789042624] %
+
+Mass Used: 2528.0301016677718 kg
+Launch C3: 59.52876507974255 km²/s²
+||V∞_in||: 7.3400791119043935 km/s
@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EMMJS_2021-12-03T14:06:15.707/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-07-25T10:56:35.081
+Launch V∞: [-0.946994040198373, 0.7451481404956214, -0.8183806644150764] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [0.014258156666681189, 2.7730331960192176, -1.1269036535413253] km/s
+	V∞_out: [0.5141370030166348, -0.1036905077662334, -2.9466045466696906] km/s
+	time of flight: 1.1404800000012271e8 seconds
+	arrival date: 2027-03-06T10:56:35.081
+	thrust profile: [0.9385530212613687 0.4901574978623852 0.10061758150690266; 0.963070949930897 0.8321550483186799 0.008076995378552753; 0.9477571571642094 0.9610236014179844 -0.3985885112414162; -0.8711740070381366 0.9585545422957218 -0.473960549642588; -0.35180875323453037 0.5538991572461103 -0.3047172625720546; 0.945857985340927 0.9318586412463802 0.07532442345652893; 0.916860585821232 0.9461601676367617 0.09256592206997157; 0.9203902037763169 0.9428723645501874 -0.3780093114569496; 0.1105180481588208 0.9388923575412604 -0.5467563429465788; 0.9600557668435807 0.08776536568096838 -0.6082094846555337; 0.9694071291822624 0.9576019390193865 0.042076881935371874; 0.7379014033007257 0.9676653528673065 0.20011181540529835; -0.7026385155061656 0.9228908375337035 -0.34668134552520397; 0.34660988424967165 0.77350231915288 -0.6692179888555208; 0.9672945056421521 -0.9455364762862372 -0.5850573257116493; 0.9859396795925156 0.16374570712498915 -0.26188762301350715; 0.9545064259275549 0.9869744571812468 0.4480444603786351; -0.9777686070631371 0.9725195168208975 0.193691849051127; -0.9708472634149672 0.7500006701210962 -0.37076685227103995; -0.9229893981992848 -0.9773469965294133 -0.6290625133929346] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [-0.8165677595901083, -0.06087475377585851, 3.052309046353131] km/s
+	V∞_out: [-2.9671064112310424, -0.9629127612065755, 0.5071630145897023] km/s
+	time of flight: 2.5657200000050467e7 seconds
+	arrival date: 2027-12-28T09:56:35.081
+	thrust profile: [-0.41833750150854715 -0.23745700390485924 0.5060156710931941; -0.39335607115842763 -0.21531365718730944 0.6214127928981721; -0.3741710013483589 -0.18178973996137726 0.7015878071805001; -0.3643811289828083 -0.1509347162037813 0.751160544358552; -0.3628330570779499 -0.11199271269023013 0.7793128986864543; -0.37235570205858287 -0.07302372672984968 0.7974839419031854; -0.3874662882006923 -0.03576203680036734 0.8098641766992978; -0.4074499881135819 -0.006584284581002934 0.8169150088581699; -0.4281109131913487 0.01182349039523377 0.8189971077067131; -0.4459261627474135 0.02257293277791146 0.8172972584690744; -0.4568773433902438 0.024804843226578856 0.8108158124505926; -0.4596411297003703 0.025045134417719155 0.7994526969817127; -0.4544566197190047 0.02267340988409504 0.7798827612879172; -0.44051961933116424 0.02370501075040903 0.7512234553177294; -0.41845307963023165 0.03005154105743171 0.708359052016344; -0.3881992767298684 0.04309990454210432 0.642522507646677; -0.34752334469565116 0.06138846846654963 0.5427837231822192; -0.2956992996903972 0.07742676936562033 0.40261391380265427; -0.17065939997376794 0.03880630671620183 0.2558269001777807; -0.235765575949598 0.13041638287567744 0.1404777210162043] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [-1.7554396063175077, -4.3095849115029985, -0.1325601348507023] km/s
+	V∞_out: [-4.236997629309691, -1.8724795170284283, -0.4561606000854912] km/s
+	time of flight: 1.4433840000004688e8 seconds
+	arrival date: 2032-07-24T23:56:35.081
+	thrust profile: [-0.5079766273797471 -0.10849515042583255 -0.0073545543900051516; -0.8149330561784093 0.34076004302958 -0.10326028863924017; -0.9395306205116954 -0.6895587367092969 -0.1170733748155399; -0.8439334413601929 -0.9377459623599967 0.015887598730331222; -0.12385311413264775 -0.85754750232578 0.11388747617260146; -0.15722365998440252 -0.3713893060760601 0.07983906967712144; -0.4905066367366128 -0.27630177574765263 0.052134881351611005; -0.40323969943463034 -0.36672944173144784 0.10826813939276426; -0.5166657583603889 -0.20333001707916043 0.07190841766549783; -0.9296123351360971 0.7837821870593056 -0.035789654605662545; -0.9678260619223868 -0.13908054107117102 0.11575665020892843; -0.9440698254178282 -0.9616603904467664 0.28528753638981585; 0.16941992205087786 -0.958669585346112 0.2124940591626158; 0.6017699213284338 -0.9270140863622942 0.07796374810040851; 0.39129362583737487 -0.748999519453576 0.05494281482886338; -0.005988877690288004 0.3481376434297022 0.032216440029362; 0.011527786969304827 -0.31978413035928577 -0.004592862949742337; -0.1976671384268677 0.9049682211089798 -0.21479203411765663; 0.5371991705488778 0.9049363560121139 -0.175235712765763; 0.054168546279189246 0.9414663774468465 -0.16207020976741393] %
+Phase 4:
+	Planet: Saturn
+	V∞_in: [-6.539365214334455, 2.218176712783986, -0.36626020172775725] km/s
+	V∞_out: [-3.665136112061718, 6.451338183645968, -0.16457889689277141] km/s
+	time of flight: 1.812492000000014e8 seconds
+	arrival date: 2038-04-22T18:56:35.081
+	thrust profile: [0.05264623774997263 0.215338495237562 0.003754114844726852; 0.021165626937991143 0.22155170870739663 0.0047677855635804905; -0.0033929172288595286 0.31227924099890236 0.06539164976806457; 0.5694561518181592 0.6749368464572498 -0.11566610061632827; 0.1324891033231393 0.3597380526244606 -0.022962295545894153; 0.024627138889422973 0.3245686299565964 0.04183403216303953; 0.04019245536713721 0.744671990758876 0.03457514031015897; 0.03322017112484851 0.09302676824184232 -0.04257715628694308; -0.5866822473952952 -0.1769325756395129 0.23680697649509092; -0.14301190082784437 0.09180461385600784 -0.028924399094075886; -0.18983362654037655 -0.01602479614573261 -0.1446728759943558; 0.17123430049602928 0.2161630553091436 -0.12107554476977027; 0.0336023230656082 -0.34829018802826484 -0.06164799648134331; -0.0137744016652137 0.032090633273540385 -0.01461460357642287; 0.023301081130224558 0.023046782785575825 -0.0014039211755592525; 0.04517905715080291 0.07387132921915998 0.025233349143655093; 0.019815422280705618 -0.054453865039265595 -0.04881233646684176; 0.010800262146714945 0.40350474993323376 0.07282207796248781; 0.06922178100116284 -0.38131801494106843 -0.09824591875105594; 0.3129500615782364 -0.8033474844184223 -0.09841107223379629] %
+
+Mass Used: 2769.31857214896 kg
+Launch C3: 2.1217903753437817 km²/s²
+||V∞_in||: 6.915038096131817 km/s
@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EMMJS_2021-12-03T17:38:37.546/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-11-08T16:33:41.148
+Launch V∞: [-3.7467429728623447, -0.7427414062360022, 1.0452490382459865] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-2.885104439331886, -1.327495046167686, -0.027749058108596784] km/s
+	V∞_out: [-1.635967097498029, -2.7221789573242074, 0.015131202359034032] km/s
+	time of flight: 6.778595425260136e7 seconds
+	arrival date: 2026-01-01T05:59:35.148
+	thrust profile: [-0.05074044407568138 -0.021150582055882192 0.02730812822478398; -0.05363696950139044 -0.06016484582924907 0.04378542458137859; -0.02771035674834004 -0.10645426057233084 0.04017412625773127; 0.01630657360103497 -0.12411195034078264 0.023350505322999197; 0.05888817282501315 -0.10894637011686983 0.0004869417342207616; 0.08706942097452976 -0.07439720218837492 -0.023367157675286705; 0.09495132401480658 -0.035316011414834675 -0.04390702621881143; 0.08752285351021441 -0.004210304140208955 -0.05824943912322043; 0.06832834450779833 0.01653042551161497 -0.06490194085584605; 0.04924860864138059 0.022800133521631457 -0.062427366917489194; 0.03691868046224741 0.011541999666891671 -0.049506900069146154; 0.02451718791619906 0.019175805931995835 -0.026347851368135194; -0.032064249204675696 0.028639492606652335 0.024093899166278167; -0.08306772663523894 -0.03165903417995458 0.04031997576998134; -0.09308798794042389 -0.09539353910087413 0.04749994325844049; -0.02511528438762353 -0.14606890192307997 0.03354911283916682; 0.04310668443858089 -0.14207536740537 0.010418445496805094; 0.09246132545360927 -0.10807413652564378 -0.01547233992587798; 0.11319881808511016 -0.06123358244390861 -0.03864051024951101; 0.11067805251913554 -0.018856574108340608 -0.05612659024233843] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [-5.884459586892747, -3.363236848676117, -0.5090555323000778] km/s
+	V∞_out: [-6.754575036027653, -0.6433971508597986, -0.39980914727121014] km/s
+	time of flight: 7.419247222558242e7 seconds
+	arrival date: 2028-05-08T23:00:47.148
+	thrust profile: [0.09654790671377476 -0.02421154193760562 -0.017928801450145315; -0.013697559588275829 0.2078634802144036 -0.1014668129386949; -0.1556430254864518 0.42999351341524117 -0.15436045217579106; -0.34594668129342293 0.5414366154963298 -0.18269379097659816; -0.5454038742991185 0.5440039323636802 -0.17114242041739094; -0.6681265735588777 0.3905344944333295 -0.11698706816633163; -0.7178501053667702 -0.2147414683533294 -0.03563087595180013; -0.7220121820048746 -0.6387659476154413 0.04867755848318845; -0.6341573780307701 -0.8263426625319585 0.11250663825239217; -0.42165856247956973 -0.9426406733296913 0.15700663915570923; -0.2282676099099079 -0.9148864509029049 0.18224086165253006; -0.19975433285802874 -0.7643878036213333 0.18722809378704905; -0.23887594019854455 -0.571448552171104 0.1698384408589319; -0.20476059817742176 -0.3599675936442139 0.12804247162016902; -0.021622630852921543 -0.18516594772639078 0.08091546982169469; 0.06780313268150127 -0.07159692617114882 -0.012001883119840365; 0.0737246732088521 0.19689739773217652 -0.0905687562910174; -0.07537764165798895 0.41078706656960723 -0.1422877828900227; -0.2938291349463374 0.6466716586743462 -0.17361703816996657; -0.601397213043171 0.6791254738338734 -0.16212519541868492] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [-4.520674651049057, -2.5409484551232677, 0.26037246970875744] km/s
+	V∞_out: [-0.8008259820354645, 5.108593255783271, -0.47079137990954545] km/s
+	time of flight: 8.970106359744217e7 seconds
+	arrival date: 2031-03-13T03:58:30.148
+	thrust profile: [-0.9144771548791947 0.6902760792706399 -0.02961910274543401; -0.9666896369671112 0.2364932018447611 -0.03360017687916256; -0.9297691297960539 -0.38607984447798555 -0.01355789584429883; -0.8346154484217878 -0.6214014693922587 0.0166085094653681; -0.7129033965945708 -0.700963733220583 0.041959359935916686; -0.5741438889568534 -0.6419595568492229 0.05459259074755743; -0.43236122782537784 -0.6653422888597984 0.06339767277888375; -0.32424450019548473 -0.6113143615391297 0.0649952740051996; -0.2507213613172347 -0.5715625368541332 0.06495239951441104; -0.2066973617297525 -0.5173029196105642 0.059981187403511056; -0.17530451342656214 -0.46356648825594077 0.047624841826828745; -0.1477866838400433 -0.3897245825635479 0.049242714379565865; -0.12010797428356033 -0.31542712311456955 0.03834216234998446; -0.09300258495305348 -0.23794128216440627 0.032748124103639975; -0.06465067006435225 -0.16076271327460043 0.023845385656830805; -0.03888290411251017 -0.09081101903598543 0.01503347691667522; -0.012590046428086619 -0.034506030314933926 0.008899905471236012; 0.011376964842136187 0.007648534577971764 -0.00016213377538379614; 0.03978470139669819 0.0415658896303641 -0.008546043818250205; 0.05975267589922902 0.07118967492032456 -0.006512156351974285] %
+Phase 4:
+	Planet: Saturn
+	V∞_in: [-1.3584481648257494, 2.8741322587661022, -0.2546304125259141] km/s
+	V∞_out: [-0.03780230346481573, 0.0035967292583968646, 0.0007694792047629233] km/s
+	time of flight: 2.6826096516036582e8 seconds
+	arrival date: 2039-09-12T00:54:35.148
+	thrust profile: [0.15488733950530229 0.004571931625674222 0.014146553973814535; 0.1553899576809856 0.03891862438324717 0.011973507362994223; 0.14041589251623252 0.07646409264944304 0.008869602158932547; 0.11548352038842227 0.1179485961935457 0.005517550148134544; 0.06394148482320672 0.14725938798843563 0.0012092021978766729; 0.0044327089101765475 0.13700916415178752 -0.005822274387507308; -0.029434414888955224 0.100612821704748 -0.017148622938312798; -0.033398085410118725 0.07353093978663178 -0.020258407230342786; -0.022858879964930717 0.05475230911401911 -0.0235821272789971; -0.013323435304460137 0.041377292100863744 -0.02450308078568975; 0.017138449993525783 0.0028560178783815105 -0.007160323142177257; 0.001062473462116934 0.0017720804053553297 -0.03347589005736904; -0.005736640138015923 -0.01153596653687124 -0.031458002877494486; 0.0015233910519389863 -0.004860382970013982 -0.028357121836203404; 0.006148876075267932 -0.01671721636961961 2.8524011567020264e-5; -0.0025972753111940814 -0.024320445695816754 -0.02183259610480299; -0.011337447226728808 -0.029412701131799595 -0.010842354984299675; -0.008925944814787248 -0.03382785337511997 -0.002144952702459933; -0.002362954309468288 -0.03692199124600801 0.010934038390259249; 0.006643709781956786 -0.044837750975252416 0.015646911234478936] %
+
+Mass Used: 971.9203240703632 kg
+Launch C3: 15.682293253184955 km²/s²
+||V∞_in||: 3.1891776846675537 km/s
@@ -0,0 +1,29 @@
+archive/EMS_2021-10-18T16:59:17.315/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 2500.0 kg
+Launch Date: 2023-04-28T02:09:03.278
+Launch V∞: [-0.28345133710132847, 1.0743854420236858, -0.7978154104086252] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-3.9967794624862174, -1.796615553688495, 0.18069271269193854] km/s
+	V∞_out: [-1.548984364644081, -4.0995103503572965, -0.1751138267279006] km/s
+	time of flight: 7.294333712413637e7 seconds
+	arrival date: 2025-08-19T08:11:20.278
+	thrust profile: [0.27129342959528535 0.3105357481410173 -0.13776198909539616; 0.2857943315505697 0.37422284577893283 -0.07741685575269751; 0.29147675327956785 0.43700523965167776 -0.03795847200581804; 0.26195889887210855 0.5028181624971211 -0.0005396605815887358; 0.15264241517349655 0.5627027239358379 0.04026796082311949; -0.21472716598613734 0.5656221884285355 0.07589844603666616; -0.44097859377494264 0.6011415225988948 0.08882761279301371; -0.5596322482349072 0.5924790276186342 0.10349315642725657; -0.6494338922092608 0.5147834423861947 0.09878164045059151; -0.6890853276610861 0.34769944485046655 0.10758903353087095; -0.7017547619444012 -0.20057354620150453 0.09920813690355593; -0.6745685731946026 -0.47742479501621643 0.07312125071193376; -0.6142120609058455 -0.5797834769079339 0.05733530776830226; -0.5194160499914027 -0.6309171109593869 0.04757759512967653; -0.3492605663341956 -0.6402207247189663 0.041146835896067636; -0.03951993531458719 -0.6527963719677305 0.03181129156545075; 0.3274132441095414 -0.6019543607111664 0.027166201765400827; 0.4453849819849971 -0.49234605468138865 0.05074512372671259; 0.5656848679322919 -0.39420475408757977 0.0050941306261821; 0.6326427870763563 -0.00451471603294776 -0.007898661242615889; 0.6344442066851826 0.32653453932748283 -0.009015317754992064; 0.6158812059226126 0.5177117651296143 -0.008708549103931514; 0.2766392824421838 0.6376517469055978 -0.007044397327081956; 0.48635720454238257 0.7015258666642404 0.005391023657919901; 0.2388275095993961 0.7839703160185039 0.0237255785528516; -0.34777254471610497 0.7710290576451031 0.03551844333501986; -0.5885930858213723 0.77414168676162 0.04420044290731061; -0.7164444323934833 0.747056729582095 0.05363112099094788; -0.7783931094123401 0.6945452939195893 0.06286922516715199; -0.8067126938364534 0.5559766275710116 0.07072695146073339; -0.8142556813471 0.18799458490346557 0.08295945452803895; -0.8237609785746686 -0.4171222798419635 0.07484624641818867; -0.7811394140789718 -0.636438184214109 0.06873112603384107; -0.7550230629750426 -0.7150279828307937 0.0684978024408926; -0.6940899011304569 -0.7452234816802559 0.0735184431000053; -0.6007177902464298 -0.7628212138609117 0.08111219954722233; -0.4481244630782517 -0.6927968720256732 0.09187154244235678; -0.18701737720212347 -0.7688281918495833 0.09508018949652022; 0.15330364620088285 -0.7571355696293374 0.10388757294502171; 0.44840462086114785 -0.7349766877868921 0.10468825098380709] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [5.478316556422099, 1.2831036594647218, -0.2967788676434742] km/s
+	V∞_out: [1.3335401352897827, -2.529320658286065, -2.9636241930342364] km/s
+	time of flight: 1.7440266834411675e8 seconds
+	arrival date: 2031-02-27T21:22:28.278
+	thrust profile: [0.8319809369429529 -0.878794436939913 -0.20832827343669594; 0.8609706878613599 -0.8267238484656785 -0.21318419084570744; 0.8656897434750768 -0.7240384649950173 -0.19979578660603495; 0.8552011838077788 -0.5064814903941824 -0.18251440493384546; 0.8363195973409432 -0.14456572446632004 -0.16593010531881136; 0.8081152165469484 0.18808739340507105 -0.1487369487997654; 0.7768813112799857 0.3321030569792334 -0.13271000839154282; 0.7461547816325443 0.380535079147646 -0.11963434440133103; 0.7336370612568931 0.3876085937165446 -0.11374822501010452; 0.6722438478009509 0.37262354402865455 -0.09924635260998549; 0.636700827451306 0.3482750141362841 -0.09096263174423401; 0.6000979234400551 0.3154896668797045 -0.08347355473204951; 0.565321980717556 0.28197409120639905 -0.07679574071779935; 0.5362347487863641 0.24879840786012403 -0.07052526407699661; 0.506456983388694 0.2178916113871946 -0.06484065560897957; 0.47867392861017327 0.1895873664700829 -0.05934971442801367; 0.45188546802743645 0.16483989816565228 -0.05428532815991076; 0.4258576643452032 0.14314351622849766 -0.049453046387159375; 0.3932180809584342 0.12600938110354004 -0.04515398008512076; 0.3736000015785295 0.1093387430388073 -0.04064878570403887; 0.34746834593741427 0.09663389153595585 -0.03657445916446597; 0.3263804706557932 0.08143119972171763 -0.032253660229846555; 0.29446796677601816 0.07716255241477146 -0.028952185397828487; 0.2675603950018661 0.06913068815160486 -0.025416936036410424; 0.23935147926901057 0.0638464827639863 -0.02232743826164184; 0.2112515499774626 0.058296071404257035 -0.0193898963172417; 0.18154839012996993 0.055479572083340103 -0.016490357086754774; 0.15178288263458828 0.05251212884747476 -0.01386116412051058; 0.12169795930534069 0.049695122256651396 -0.01143496736298545; 0.0910474586010959 0.04765355590466685 -0.009254813498398738; 0.06032007090632702 0.04588860726880914 -0.007296428456263087; 0.024177392897664348 0.055877005503225545 -0.005013775264453432; -0.0013205135851091791 0.04362298856063178 -0.004342404637589318; -0.034268981603339986 0.04171264705427312 -0.003016390318187484; -0.0599598695163209 0.03777860828611642 -0.0011051873513641581; -0.08396131013198456 0.04004076835062581 0.001289908726025911; -0.11237838352227249 0.043118231503448255 0.0038935225675295515; -0.14192940631843057 0.044900767830437484 0.006105003050706572; -0.17249363934725057 0.046526921854485405 0.008060655464185872; -0.2031778124949161 0.04704983155445407 0.00996707335341186] %
+
+Mass Used: 1099.5265655762369 kg
+Launch C3: 1.871158167622445 km²/s²
+||V∞_in||: 5.634393045358124 km/s
@@ -0,0 +1,29 @@
+archive/EMS_2021-10-18T18:22:44.188/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 2500.0 kg
+Launch Date: 2023-06-03T18:39:41.030
+Launch V∞: [1.4528171939898546, -0.7402553543714421, 0.7198063620664785] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.09755558196699422, -5.3760255002748165, 1.7853084087216329] km/s
+	V∞_out: [2.8879492524068695, -4.6008182394117, 1.6098548998016842] km/s
+	time of flight: 1.362669505585263e8 seconds
+	arrival date: 2027-09-27T22:35:31.030
+	thrust profile: [0.014609011290562383 0.023526054638363506 0.06586887507050274; -0.06429218902505592 0.0003875221488966037 0.025068287312389175; -0.07722181604763545 -0.0164935736357545 0.006484354491785095; -0.05418670199657678 -0.022646287453370457 -0.08113490766539934; -0.0506166491243181 -0.04748837806503002 -0.10084803864225915; -0.06035477738922144 -0.05527195771007038 -0.11674201815059983; -0.08962934751172418 -0.07120699904034963 -0.11701738451143721; -0.11623494873904305 -0.12424723770859708 -0.10180855594746802; -0.10825232081959534 -0.20934236634778766 -0.061949505438447156; -0.04450437764051239 -0.29053535177066586 -0.0052401903439667245; 0.10858287109159012 -0.33531112320191925 0.050573299933059424; 0.2917560473211387 -0.28130087234888473 0.09141235049602812; 0.363552744102322 -0.0653888495734924 0.1119765464717816; 0.30023433762797985 0.1586653839712532 0.09775032797542846; 0.13381909610838597 0.25349442292502145 0.050962207120256495; -0.05561879073077972 0.25047891650044996 -0.010222224987169614; -0.18500289408520745 0.1838459648234384 -0.06501054068816181; -0.2633626984585559 0.06740350331400906 -0.10552803707472241; -0.3015544455362966 -0.08340867428702191 -0.12617391907275552; -0.2980095390699629 -0.2392946380342424 -0.12629505951265152; -0.23148023546107505 -0.3749701410683523 -0.10783217167181713; -0.07894071469307276 -0.4623486266693046 -0.07144480401887415; 0.16028862146595801 -0.4876815213223878 -0.02061179953627845; 0.3842493049278076 -0.42962504947168956 0.03643143668725137; 0.4974283466407711 -0.25309214932909857 0.08670208210950218; 0.5081883636716127 0.056291903479390164 0.11796471433830415; 0.4250685878142111 0.3104706473083573 0.11729541002445289; 0.23197825493691604 0.41240232472252586 0.08768881929972193; -0.0341851598132791 0.4223722506927382 0.03849582457917256; -0.24433348749555175 0.3610375051148529 -0.012354553480072056; -0.3655218556786849 0.24731588669440885 -0.05623949962000103; -0.4321022352880162 0.08131757252852433 -0.09105682922783279; -0.4452688895396858 -0.1283039646949706 -0.10285727576535383; -0.44828910931376825 -0.33298162270769677 -0.09536559717749803; -0.38974387016899464 -0.4806378526366322 -0.0761592904485703; -0.2542461950012492 -0.5780829896901187 -0.049525518351972206; -0.002525096494219299 -0.6161727076821379 -0.01995455750679716; 0.301010770990131 -0.6164209241411417 0.009878755441330631; 0.5087877254811393 -0.5664346000510313 0.037058328078365066; 0.6087744242184348 -0.43501726760054543 0.05873876234455045] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [3.5677789156110467, 2.7323128411776048, -0.5598992896398332] km/s
+	V∞_out: [1.0115880934192722, -1.8761487227720552, -2.6595170315286336] km/s
+	time of flight: 1.920830007442836e8 seconds
+	arrival date: 2033-10-29T02:58:51.030
+	thrust profile: [0.7881817473912547 -0.3389570569515258 -0.0694603003835884; 0.7545518240816476 0.16890824057359943 -0.05140667750465577; 0.6716820532694702 0.45119947667699334 -0.040831401900494044; 0.5658986867834962 0.5296028081006117 -0.034430918767449886; 0.4601436552292838 0.5475873435366672 -0.029817337051142707; 0.37050165220345244 0.5161676453402835 -0.025404500044545482; 0.29817541281347015 0.48289541289681487 -0.02110019963638442; 0.24169921197011807 0.44481524027189223 -0.01678514557739015; 0.19799125176255297 0.40636791170350123 -0.012722544258577625; 0.16428420463735924 0.36992082529127546 -0.008920457561270273; 0.13698227078716912 0.3355724366720239 -0.0053512238222314734; 0.11629130909242422 0.3060842336647084 -0.002489926881812709; 0.0987526125187477 0.27798808469115466 0.0002579142494755621; 0.08496841699409616 0.25449290869954533 0.002544966213217921; 0.07231123011723056 0.23076223747312233 0.004936145151231231; 0.062055600081047414 0.21341224350289537 0.006970017100223167; 0.052971371729138676 0.19639984729795226 0.008912261502883554; 0.04491958739793588 0.18126531579006996 0.010694634190802039; 0.037516267473304735 0.16812010997359988 0.012304447489889469; 0.031205986014880224 0.1567127760397761 0.013579987889275308; 0.024964383575319944 0.14503758963145616 0.014795695571499715; 0.019486740557152424 0.1362257015826171 0.015574564807330962; 0.014158411905557245 0.12789681805235922 0.016125715357447532; 0.00908308339622475 0.12028286897448305 0.016371544848018692; 0.0044102283095267085 0.11345559090550508 0.016294319554773354; 0.0005966776869157249 0.10751884153271778 0.01572311388373797; -0.003970105448958323 0.102279781501889 0.014937124392557143; -0.007640861057492033 0.0975984328130423 0.013618238849724724; -0.01144277898857823 0.09288700411779988 0.01215176103351869; -0.014785099224280838 0.08873083508061831 0.010231512465192402; -0.017730681821126432 0.08523320581633666 0.007925597342036909; -0.02102250152959055 0.08175375259513366 0.005511476561201909; -0.024837202491318048 0.0784357240142721 0.002989652933139063; -0.02916815773485098 0.07561185185811473 0.0004038081994905193; -0.03510340581821502 0.07180740263170013 -0.0021818331399174945; -0.039579141117804674 0.06726211579068186 -0.005175977417815043; -0.04013452158968421 0.06358356010989077 -0.009080952414709772; -0.03743321426527317 0.05894746602403381 -0.0148014675802013; -0.03482398229591096 0.04786083701811494 -0.02059203468208998; -0.034121069580906806 0.04002789158453891 -0.017780319292331873] %
+
+Mass Used: 844.8639343830812 kg
+Launch C3: 3.176776987699523 km²/s²
+||V∞_in||: 4.528583339995187 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-11T12:00:40.323/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-12-15T15:53:57.209
+Launch V∞: [-8.799630990613117, 7.34551872539945, -0.01567157263418129] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-5.525424782477056, 4.4780198756447795, 4.819122758622572] km/s
+	V∞_out: [-4.706421743487455, 5.965879679145328, 4.008068881526253] km/s
+	time of flight: 3.454176957567771e8 seconds
+	arrival date: 2035-11-26T13:15:32.209
+	thrust profile: [-0.3626481337773754 0.04577398887343224 -0.01655095159279829; -0.2591029103072647 0.1372224625894388 -0.03484794687568234; -0.22866525688135636 0.17047902428739029 -0.04398596135663903; -0.20591128156544064 0.17475285966822163 -0.0492888779248724; -0.18150056503077222 0.16778930777145082 -0.052511568277184374; -0.15335231896039642 0.1563088671676009 -0.05489695682401099; -0.11969538605349696 0.14368122907327513 -0.057381477632554384; -0.07554857095074854 0.13274289955008667 -0.061134164848177484; -0.005662845372976561 0.12158533590493402 -0.06883945566112469; 0.08882737363292448 0.08080812675137844 -0.06713978489287248; 0.14973273476648047 0.012685076152274712 -0.054648024648829695; 0.18323594004050148 -0.016384245272972057 -0.040066936961717516; 0.214348858008005 -0.03857066861559532 -0.03192224738926298; 0.2437677883438544 -0.05412293733006518 -0.024660532031911552; 0.2708260597859475 -0.0661687448280918 -0.017461136277209074; 0.2929814040329991 -0.06841327312791493 -0.01010361901238175; 0.3092263370993894 -0.06754436134630445 -0.002601950724966861; 0.3149711596447107 -0.06392107998759775 0.004480656365829517; 0.29966216490402514 -0.07283217119754073 0.007976136077309862; 0.2774497080818675 -0.23673465946359637 -0.020355523705770436] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [-3.3584183538877763, 3.8318829241241077, -0.7567106147040691] km/s
+	V∞_out: [0.1021866916167663, -0.00023345092684676295, -0.009051525807691481] km/s
+	time of flight: 1.543622855088476e8 seconds
+	arrival date: 2040-10-17T03:40:17.209
+	thrust profile: [0.13343967665884301 -0.10506545000498568 -0.0477351077659778; 0.1302117419653648 -0.03935460102717447 -0.05153213061680276; 0.11177284747102363 -0.01257220530234715 -0.04992659428886335; 0.09652693312293067 -0.002381618439009866 -0.04765269265520941; 0.0850825371473891 0.0014317391384792745 -0.04538853860191621; 0.0764692224980894 0.002389375863760724 -0.043313336682117246; 0.06984581101704013 0.001982743995643555 -0.04109653594773106; 0.06469926152021455 0.0007704842623266529 -0.03917176815195523; 0.06065861914276538 -0.0009274805284651806 -0.03711303987104724; 0.057503566679394116 -0.003082072948930367 -0.034909201620028106; 0.0550645718937643 -0.005650610120539781 -0.03268940722476422; 0.05322150250858926 -0.008613752406916884 -0.030366444716783268; 0.0518961775636053 -0.012130900432895326 -0.027730459432375138; 0.05102478831673343 -0.01609208695110308 -0.02458927158108588; 0.05053365271120057 -0.02060666132173175 -0.02046187508115701; 0.05010304886930772 -0.024812286823873268 -0.01532028206532522; 0.04934671183992039 -0.028238984577646484 -0.009343074776168988; 0.04800853819288795 -0.030411131488611035 -0.0034811661314590016; 0.046080118190868546 -0.03168857673917387 0.0018689351571204262; 0.04350626131303775 -0.03258848698710888 0.006743047916297395] %
+
+Mass Used: 794.3057297478713 kg
+Launch C3: 131.3903965143416 km²/s²
+||V∞_in||: 5.1512048627801645 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-11T12:46:58.095/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-27T20:44:12.105
+Launch V∞: [7.331043976806805, -1.4831196012007795, -2.0245623512046933] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [7.494654195262718, -6.0609925282532195, -1.5465164285364046] km/s
+	V∞_out: [8.361426259111628, -4.4394354885497, -2.3823072505126612] km/s
+	time of flight: 1.0927270179201613e8 seconds
+	arrival date: 2027-12-14T14:15:53.105
+	thrust profile: [0.023332265026031952 0.009104569108764901 0.00629954147585845; -0.0016557218791188077 0.01962631342128255 0.025705762368190936; -0.024093977262103067 0.034136267923482864 0.04127784193457851; -0.05716526136359704 0.04151655990433137 0.04937581881860671; -0.08978841140825183 0.037467471815706095 0.04965327321348644; -0.11993513223616677 0.026533967699871562 0.046755622510516306; -0.1531417398423054 0.011465166956525712 0.0450015339745295; -0.1798910024661249 -0.010958035234353167 0.040725164468314354; -0.19949258297853104 -0.03912791834137119 0.03496282370942105; -0.2095378189457459 -0.0715570982112501 0.027651575768606357; -0.21854976076053584 -0.10808558698891595 0.02118335219201054; -0.19007677121186733 -0.14660854579446153 0.009316164763448933; -0.20623923432304714 -0.19574889973495846 0.006342495476503129; -0.1946190022918896 -0.250488140357656 2.0902619062690796e-5; -0.1631047479714882 -0.31008060921369185 -0.007131331834578688; -0.11255143746171749 -0.37370964738271606 -0.013811169750461278; -0.019515019669034205 -0.43369153744750616 -0.020445519976909028; 0.19816480144351972 -0.44821129856705755 -0.03362906769054827; 0.5110188524621195 -0.31112343771146783 -0.05819048814446341; 0.6288004165000244 -0.04917320571657702 -0.04513050099902747] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [5.293734358571078, 2.8678408184561692, 0.013339550220484931] km/s
+	V∞_out: [0.04716000390909402, 0.22366680587637539, -0.5447644595624558] km/s
+	time of flight: 1.425235096053826e8 seconds
+	arrival date: 2032-06-20T04:07:42.105
+	thrust profile: [0.6576686143235253 0.3983282167692387 -0.040657820784520814; 0.35898947395338654 0.482213895760015 -0.01457736331055029; 0.2418918180398632 0.40917465296239935 -0.027235944158173563; 0.18693029836434163 0.3001309863445353 -0.04795078143893266; 0.17245763177523526 0.24020298673049806 -0.04814251518646192; 0.14210932515321834 0.1971999216967911 -0.04644978179421798; 0.13551601813035644 0.16075235436433832 -0.04687487556492608; 0.10999571544133116 0.13945505978150918 -0.04018977645283118; 0.09389237369435716 0.12249824726225744 -0.034147954132379775; 0.07817603467998095 0.1091061330560275 -0.027512895131446207; 0.06000859121748583 0.10654100938138575 -0.015903939946752932; 0.044248657050263394 0.1002027939962748 -0.0037526170023857133; 0.017432466468028006 0.09844081095460211 0.015736280260922626; -0.0028322518503023707 0.08407047604089865 0.03216268095410213; -0.009665030744853838 0.05418448600092389 0.054271394924132535; 0.00829991223524997 0.03671735113395197 0.07037788504936107; 0.05287971274655226 0.010024909695991463 0.04123949561959472; 0.03098994422797628 0.013396671609721751 9.284814456508857e-5; -0.002877075807447608 0.0005192110683645124 -0.004545971900385684; -0.028522171379334084 -0.019564193850904677 -0.005660284903915027] %
+
+Mass Used: 462.9647257745969 kg
+Launch C3: 60.04270225525677 km²/s²
+||V∞_in||: 6.020657137117126 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-12T02:20:38.349/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-27T01:02:22.769
+Launch V∞: [6.7386630924747735, 2.681719926533396, -0.33192262753473517] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [7.715602805644678, 2.5340401706785007, 0.59216879433437] km/s
+	V∞_out: [8.14158010025008, 0.11467559822796293, -0.05931443388440504] km/s
+	time of flight: 9.561374944761689e7 seconds
+	arrival date: 2027-07-08T16:24:51.769
+	thrust profile: [0.023301022793894528 0.014506194191639996 -0.0023755438375060796; -0.0033183751580871247 0.07336782130026553 -0.010811507865922472; -0.06164727407552523 0.1056496969546475 -0.015161235314008188; -0.11620137406382157 0.10874515644970927 -0.01361354605050158; -0.1601570651283726 0.09921746096307649 -0.012671822225267419; -0.19082531605807282 0.0802558926347972 -0.009996142143905916; -0.20208459146376992 0.05645991756914749 -0.006506293164629694; -0.21544032645611308 0.03523333870753496 -0.003351285055413982; -0.2146729665158058 0.015989911852492572 -0.0006952731036961628; -0.2100243756555401 -0.002329651168066605 0.0017750081369577472; -0.20068199973477896 -0.01650191290529539 0.0032462994310995894; -0.18569841958374314 -0.029823004573719693 0.005192162167569715; -0.17068555643039118 -0.04088645007952001 0.006882136983000742; -0.1544233058448683 -0.05266519452045455 0.008779360398481333; -0.13772295301894258 -0.0660836116852668 0.010909532136160287; -0.1245197103734167 -0.08412870453765404 0.011561357511009963; -0.11864715197412816 -0.10345797348459172 0.012266842139150844; -0.12286715595935756 -0.11968342646377855 0.013379062014771508; -0.1280643838181201 -0.12655169696513147 0.014368799422308797; -0.0584121142412127 -0.09509621902471597 0.021690900981356457] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [3.8395108661970547, 1.7159262299086049, -0.5755224531865024] km/s
+	V∞_out: [1.585491120038796, 1.6910585908232016, -1.5486076554083772] km/s
+	time of flight: 1.9541956884803814e8 seconds
+	arrival date: 2033-09-16T11:37:39.769
+	thrust profile: [0.6823696785602157 -0.17465970925833899 0.0043786960922660234; 0.6324817977952034 0.37687729714593043 -0.01591902686901882; 0.3277378095890081 0.4273045997113089 -0.028355410420497114; 0.10029194711800075 0.3999364225521307 -0.03982802930015918; -0.020337081717252826 0.3496704764595339 -0.0471085437841163; -0.06953931842857293 0.30506864176347775 -0.050869154269620596; -0.09029458688961563 0.2659041906755343 -0.05171965882195978; -0.09569930804632429 0.23393858191140274 -0.05045687048832852; -0.09135019739026035 0.20289486172260954 -0.0471432021452754; -0.08319328510285766 0.1751518535444896 -0.042866586306264595; -0.07234783813584449 0.14706283938140732 -0.03706890299670858; -0.06147684285523951 0.11875925720287137 -0.030811114879888888; -0.049301448626872475 0.0927610035215594 -0.025105771012088114; -0.040797799440948385 0.07229409923332282 -0.02206113454900311; -0.029504166236854465 0.034043477456934826 -0.01610127680367871; -0.026224768748220457 0.020043015937368583 -0.011941084397735483; -0.02324819576509405 -0.0026427941112453753 -0.03949368883582122; -0.02103554091162609 -0.0003860869927297471 -0.016902655236921048; -0.021394310561898423 -0.019531075903377628 0.0019258727279209144; 0.004724715524274068 -0.038805914811576483 0.005891653322046331] %
+
+Mass Used: 495.51091656724066 kg
+Launch C3: 52.71137466891752 km²/s²
+||V∞_in||: 4.244699354754754 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-12T14:59:57.936/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-10-25T14:05:40.189
+Launch V∞: [-2.237183685934752, -2.721647916047431, 1.299312276740919] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.678207962240434, -3.5504123945109747, -1.2418379495810854] km/s
+	V∞_out: [2.332007819175787, -2.421453655328241, -1.8183105258695256] km/s
+	time of flight: 1.855655995918323e8 seconds
+	arrival date: 2029-09-11T08:05:39.189
+	thrust profile: [0.19727184520667015 -0.3838952007487214 0.17961473110199166; 0.2077514036189871 0.5200804821813247 -0.10558577682756237; -0.022196502289827003 0.3282119359443656 -0.17880640948902576; 0.022167314146114503 0.3526089664383984 0.35012764112560996; 0.3025719335339175 0.3093777519487111 -0.17023625811931237; 0.15995107289139296 0.3622712142968187 -0.1750157659189659; -0.2760617452549359 0.41412522749535996 0.17764253337734176; 0.32935922189339817 0.1968557028627668 -0.026495445347781893; 0.2681770910187345 0.4086838063855519 -0.18928477304761748; -0.24197868619321736 0.45257178565912115 0.10670805906910212; -0.30369774778452496 -0.386093378582689 0.10490688892166344; 0.5108677715826049 0.1835799494496108 -0.2034993601786804; 0.045093348543829 0.5895547713851573 -0.034986947864212484; -0.5736310275454822 0.23658188722553572 0.18619609441669782; 0.23133883855583576 -0.5862475003689892 -0.05214808227492976; 0.6442849903188875 0.40530400231961805 -0.21464210977314127; -0.020964246471072177 0.7236236640594544 0.012492389285940016; -0.7227867443191269 0.34102536963229013 0.22159525812592265; -0.39003244325739894 -0.719098783178554 0.04735599030806113; 0.7348700748588787 -0.5860442405640622 -0.2239590199604165] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [1.2532005419075063, 2.905447896432199, -0.443912289899149] km/s
+	V∞_out: [0.009293489123982904, -0.022791627564424932, 0.00035910126775256265] km/s
+	time of flight: 3.841884000189513e8 seconds
+	arrival date: 2041-11-13T23:05:39.189
+	thrust profile: [0.8354818174826176 0.8278651352879969 -0.019139799616379415; 0.07789587464121626 0.807772028598289 0.09208866935020069; -0.4371258372752062 0.7097083046464899 0.07648931927262204; -0.4593926819327141 0.5921013650423435 0.05279771473551259; -0.41803959049762845 0.4756823109687688 0.03511376028590402; -0.36046979629046133 0.37325588585291325 0.023223381248584807; -0.30164482520132996 0.2891579617780395 0.01559727222329367; -0.24852711164559912 0.2211224649200195 0.01083260426477029; -0.20341018128087673 0.16521746219046313 0.00787777038183007; -0.166313250377776 0.11914245715911004 0.006052029723090913; -0.13685498996724776 0.07579955310252746 0.0051696709685845; -0.11590045234482386 0.03683619622380138 0.005503034114011019; -0.09714808717387836 -7.510913642337649e-5 0.005881543716786649; -0.07947906741787436 -0.03636451674166609 0.006573855151556507; -0.060762284460828354 -0.07185315172378559 0.007324504256710228; -0.040146440269578795 -0.10503734607332527 0.008063012601483146; -0.01826447390719847 -0.13480682166408572 0.008650026851941802; -0.0014999731370244022 -0.16167322260227676 0.010344109911906468; 0.019647516899938273 -0.18187401707529088 0.008884133379429506; 0.07031314483210122 -0.20333200721827405 0.010747903674476903] %
+
+Mass Used: 1995.6659445951054 kg
+Launch C3: 14.1005706160276 km²/s²
+||V∞_in||: 3.1951834373386236 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-12T15:39:06.197/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-04T08:15:42.979
+Launch V∞: [4.591627441054104, -0.9372602729162841, -1.402102560672615] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [9.367085838054193, 1.2385416703463588, -1.2664210112872778] km/s
+	V∞_out: [9.488354168340724, -0.7139124540608336, -0.5849794139568701] km/s
+	time of flight: 2.4606079841224298e8 seconds
+	arrival date: 2031-01-20T06:29:00.979
+	thrust profile: [0.48110193115514666 0.1658344957098272 0.18875138957299367; 0.2722197721770649 0.41958962982537107 0.2031126777241352; -0.14912794861230844 0.31014754435480146 0.20231048078147726; 0.41900792223774436 0.33923945509259673 -0.3410850527690159; 0.2511755140919902 0.5014702815333173 0.0058685456880530696; -0.15486070913892752 0.2360830420399679 0.2645880501135092; 0.225939307553581 0.3555635470518182 -0.2579478714227079; 0.4692868559854733 0.36449584745921737 -0.26361975800532383; 0.17776955473214556 0.5344512134705717 0.2677028115850273; 0.29341528211428775 0.25652205797659977 -0.003223292822703167; 0.47969842043937694 0.383501318717164 0.00793282457827181; 0.0557455430628551 0.42410040402941707 0.12847485289641172; 0.42501735100730476 0.4434488658095193 0.17406200336317385; 0.2586191172669515 0.3545965771776789 0.13169086497478733; 0.3994448644962761 0.3523601532459076 0.1980455999347843; 0.2712389420869066 0.2551872658044702 0.16820587889445787; 0.7160832227791448 0.05007832921773097 0.03084211842871704; -0.4014048218424198 0.4263176448200758 0.02349504793730896; -0.4648045356639775 -0.012165497397007176 0.07112680698673901; 0.3334382990840683 -0.6819542566923011 -0.05838594675754101] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [-3.033179205299309, 8.323540792555027, -0.834135394854228] km/s
+	V∞_out: [-1.7989044724374927, 4.992471036908333, 2.7395017565836506] km/s
+	time of flight: 1.343904325951288e8 seconds
+	arrival date: 2035-04-24T17:09:32.979
+	thrust profile: [0.7399454327526205 -0.5303156843529576 -0.01303320908827589; 0.8546930606858686 0.056047121557869325 0.01672326772293818; 0.8757001417012732 0.8092300745166227 0.08014191465251598; 0.7798406512457665 0.8508819508472818 0.0649883040365693; -0.03926761644682386 0.8522354272278931 0.027089526497775643; -0.434264020033893 0.8459075469832358 -0.0040464336106154335; -0.5548067523933243 0.8328498997908219 -0.030544100084358417; -0.5947401029696081 0.8138198308943535 -0.049034191658682065; -0.6075585777480846 0.7820903525414267 -0.062173373203187395; -0.6029505069844785 0.7335072879202299 -0.07007906442079202; -0.5799580021535939 0.6730106758444432 -0.07459794494237851; -0.5482338658185978 0.5906864307437136 -0.0756851978219243; -0.503124125207766 0.4976084605014916 -0.07059787047969154; -0.4525092012219953 0.3942979609123233 -0.06424348023914521; -0.39298962065606696 0.2862145343873863 -0.055308865576020064; -0.3253259710648706 0.17741161874473715 -0.04466835734562229; -0.2605713062487545 0.07474580225090127 -0.03489801748303663; -0.18829323187093158 -0.02019200756889348 -0.029721867673255048; -0.12407983907216594 -0.09176887331289074 -0.014975937367657555; -0.07399819648159202 -0.17898421972733056 -0.0006361521051712036] %
+
+Mass Used: 1847.197572706729 kg
+Launch C3: 23.92739096727287 km²/s²
+||V∞_in||: 8.89816212898688 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-12T16:01:04.514/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-07-08T05:11:21.442
+Launch V∞: [7.608076212455678, 2.807333338029972, -0.7296465923907695] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [8.010347423561068, 3.2469372890009143, 0.9052053694493565] km/s
+	V∞_out: [8.595491836222386, 0.9305961590076297, 0.8829460767922697] km/s
+	time of flight: 1.285682951483629e8 seconds
+	arrival date: 2027-08-04T06:36:16.442
+	thrust profile: [0.07414876190498018 0.061418074622027974 -0.012644930305191268; 0.005288427050926843 0.06622341067027271 -0.01948043031768979; -0.03963858081578733 0.046911280729787376 -0.025333966766685957; -0.0693496161126329 0.031308343596909594 -0.035395597569043105; -0.09403908126205902 0.015893237291132945 -0.047093551884514924; -0.12169201205925062 -0.0007977301725099221 -0.056349298411649505; -0.13903080782532432 -0.023716664620632603 -0.06390511581051783; -0.15450668610406254 -0.04110038684733795 -0.06471664925953435; -0.15811658018787572 -0.056770227221372115 -0.06186158450863763; -0.14688366879113826 -0.06858393095838325 -0.048462199618237715; -0.12668694389924282 -0.08632300225726315 -0.034758267139006545; -0.10530920293607691 -0.10528354810684375 -0.02720399752175047; -0.09090371755012416 -0.12194843310927922 -0.021454466137421403; -0.07844574463506924 -0.1363037266093477 -0.01574716544865601; -0.05844360196093202 -0.1515941613574019 -0.009255165942420979; -0.034312300204900524 -0.16511832855603034 -0.0009688494952381404; -0.0028992408640754097 -0.17347460518323504 0.006524027611181451; 0.03968790735981553 -0.17103970596354526 0.01802812299096526; 0.09266705743272931 -0.1535778429859241 0.025140107388620526; 0.20165971230655427 -0.14421264141271573 0.040991785807895254] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [5.172452466285559, 3.681404565790302, -0.7376128757432779] km/s
+	V∞_out: [1.0471838805707034, -0.9458496802640074, -1.0540623554828816] km/s
+	time of flight: 1.3794018891807556e8 seconds
+	arrival date: 2031-12-17T19:19:24.442
+	thrust profile: [0.4631902795092741 -0.08224771535152973 -0.006480928889750821; 0.41704341820262636 0.21095659271139136 -0.02620914649646857; 0.2797622883993905 0.28592479641588525 -0.047115859690752125; 0.16999303712128083 0.27059720181308317 -0.05726221774165335; 0.10505343297735933 0.24439744913692196 -0.06242988174728664; 0.06300675973086067 0.21817544269642067 -0.06368113246047818; 0.035798514967212466 0.18835657288959481 -0.06877313709544629; 0.01319570173604884 0.17195586849080916 -0.06353926803226635; -0.0028206814647056726 0.15245841060553408 -0.06090532235092303; -0.015082533306159574 0.13455720233249788 -0.058050722168487584; -0.02467540253289453 0.11876086660610821 -0.054811640710621876; -0.03294606177558641 0.10466484376452906 -0.05156606010332461; -0.03552225607407402 0.09449768203449549 -0.04909814885511831; -0.044198382979974346 0.08219311436910662 -0.04488660247693665; -0.05192427793509353 0.07124227028180148 -0.0429911500566686; -0.06297039751477762 0.0597152997307626 -0.041771291047482936; -0.07719329504107608 0.04574422574176853 -0.04069542662253849; -0.09549593365185864 0.02256061596005478 -0.03696703906940773; -0.1044144745168432 -0.01480076697580528 -0.01798772858528922; -0.10164225283033314 -0.03637354833556879 0.00015260443811211083] %
+
+Mass Used: 369.23128366753645 kg
+Launch C3: 66.29632827513589 km²/s²
+||V∞_in||: 6.391484713856986 km/s
@@ -0,0 +1,22 @@
+archive/ES_2021-10-14T21:47:36.309/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 2500.0 kg
+Launch Date: 2022-06-29T19:16:25.625
+Launch V∞: [6.0695706106569, -1.6109289130217384, -0.5333379447287113] km/s
+Phase 1:
+	Planet: Saturn
+	V∞_in: [4.5493209273514195, 3.4608913977285543, -0.8868908653713397] km/s
+	V∞_out: [0.2563878990001578, 0.01892815524720286, -0.25544585694329036] km/s
+	time of flight: 2.9165245490120065e8 seconds
+	arrival date: 2031-09-26T09:50:39.625
+	thrust profile: [0.14860958019742154 -0.20538020578753946 -0.0029857947830181546; 0.24425057362359953 -0.2010582389064345 -0.0022184731127427326; 0.06264366361767877 -0.26323134665411474 -0.015605032621348582; 0.1099776426723479 -0.2600231353505949 -0.07726868093658261; 0.33089491385526876 -0.40130576368271437 -0.02266361781007407; 0.29811739992127256 0.351626147581589 -0.01408132684301641; 0.10201345317223925 -0.054395098700720686 4.985459044362331e-5; -0.24365090429430264 -0.3034489310316968 -0.034487807729955106; -0.3334152550285137 -0.45649243866916195 -0.011088824883799378; -0.08095386910938922 -0.6725665822129208 -0.0006414830511198784; 0.7230355014836508 0.16667047850911612 0.022288360045254307; 0.46498186625266963 0.48480806636556717 -0.015108144063144823; 0.26260730236394 0.4260170082088822 -0.0328608028939281; 0.1457862799193408 0.3335616939365715 -0.04011809832347775; 0.1150253917004787 0.3411618936049045 -0.04313725384357472; 0.025947430647644983 0.23890044376344466 -0.04428837586570222; -0.03181842621885434 0.16589322750633057 -0.0438537282163; -0.07240941628806781 0.0912664675638024 -0.04627441978486195; -0.15565598989729182 -0.011295552314065267 -0.03729510262375746; -0.17780659953830016 -0.08636206589783667 -0.024129636397547234] %
+
+Mass Used: 860.8985796524989 kg
+Launch C3: 39.71922872384681 km²/s²
+||V∞_in||: 5.784519476498304 km/s
@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EVMJS_2021-12-07T10:39:46.637/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-20T12:58:59.053
+Launch V∞: [-8.920597561322369, -7.117372634919496, -1.472451871563068] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-5.017961509289203, -5.654947873213361, -1.4864114620218827] km/s
+	V∞_out: [-7.390394917247088, -2.021337895911062, -0.8148956710919548] km/s
+	time of flight: 4.572852817115571e7 seconds
+	arrival date: 2025-10-01T19:21:07.053
+	thrust profile: [-0.21862938814794752 -0.05580927018043333 -0.036914761844326786; -0.24413346338652692 -0.02556655529310196 -0.03840768064934617; -0.26465223193143633 -0.031988862192285895 -0.03672328500867164; -0.2775111471212138 -0.0533843665242742 -0.03463858507707235; -0.282355262314745 -0.07982445428959191 -0.033636788586472385; -0.28050912409469175 -0.10607204371684377 -0.032167717475040075; -0.2733689146909765 -0.12962521272658228 -0.03161077625553056; -0.26190711303703673 -0.14877589397585794 -0.030649321801181607; -0.24697067176434023 -0.16354203331437878 -0.029534650090164597; -0.22916216500741854 -0.1736646300332696 -0.02774354605279356; -0.20930307239303453 -0.1793556553425328 -0.02624057086532488; -0.1881341647769172 -0.18020842931174086 -0.022018620586908344; -0.16781156346033524 -0.1755305190264814 -0.017713311035217196; -0.1529314715768468 -0.16133304311878607 -0.011294101805393433; -0.1439292332041623 -0.13894686830886066 -0.005512101036767262; -0.13595373894772989 -0.11376326317155387 0.008492968124788823; -0.14161082765712693 -0.0633805633113515 0.026736612907202688; -0.14271356865834361 0.024062134302168376 0.04098391846668108; -0.1414981556176295 0.035473208118311124 0.03720171942581438; -0.13060050476893825 0.04192201790827888 0.030084566679769147] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [-9.28829223014179, -7.607789338281241, -0.2942705558666007] km/s
+	V∞_out: [-8.317437974959708, -8.663545949996019, 0.030785372299447233] km/s
+	time of flight: 5.8747531161094815e7 seconds
+	arrival date: 2027-08-12T18:06:38.053
+	thrust profile: [-0.174672404758962 0.02506293138125133 -0.02426121230831768; -0.05008204073446195 -0.07279118574621102 -0.08129060414874276; 0.18941101625787235 -0.07952903306738271 -0.10689582281590368; 0.35705302923506294 0.027307923111368104 -0.0479794442058468; 0.41799317552955584 0.12801887957214292 -0.029898349295167635; 0.4511914489377908 0.23489263829219467 -0.020213669874118333; 0.4656012050626349 0.3325378259130575 -0.014159348767163066; 0.4657014753978555 0.41280917091846614 -0.013135235235423743; 0.45029470699103086 0.4771859548843401 -0.012168900825375072; 0.4106794937152572 0.5294663391131441 -0.011594787023374607; 0.33819071474272516 0.5678785558859125 -0.010353193332547849; 0.2001630795815917 0.5937428427734591 -0.00709996654137991; -0.035108210746352266 0.6005435960325474 -0.0011602329790232843; -0.29361875930485426 0.5723600768872681 0.008300256500510222; -0.4548836328849185 0.4770722319186511 0.014296267759918423; -0.5113471724292226 0.19706675000368873 0.01697398652461365; -0.4134871925757221 -0.2340982056617441 0.01763457992701102; -0.17230637273503518 -0.34708241891449854 0.032309764753320355; 0.1190741484482409 -0.3404978442614275 0.03287368817385319; 0.30168780764812786 -0.2869031294203351 0.028403718812872233] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [-2.998311290651761, -5.22937520865022, 0.1407756821047572] km/s
+	V∞_out: [-2.856148992180316, 5.306598853387247, -0.19607428788923498] km/s
+	time of flight: 1.4159768899978405e8 seconds
+	arrival date: 2032-02-06T14:48:06.053
+	thrust profile: [0.37857744177475117 -0.5722922563923073 0.022790081593862904; 0.4498819042137626 -0.33368177218590706 -0.006756732610181868; 0.45137346520621063 0.2646268898149342 -0.06715401087102708; 0.3370898120722347 0.5147560334694927 -0.0942931710827749; 0.10406019537076351 0.6331750657513396 -0.10357703864723887; -0.3067722620848112 0.6948315815503575 -0.0862070073278207; -0.5894971893625187 0.7222874275705 -0.047061967331428964; -0.7438646368242161 0.7031736402976893 0.007847733426895626; -0.8153797919927924 0.4618300002958423 0.06963851455772195; -0.8054139924887445 -0.5908908470157955 0.097381115730603; -0.6892129370491469 -0.7264006520777874 0.08776061857832115; -0.45980277149808124 -0.7029156090490672 0.07926634239802542; -0.23430875626887712 -0.6386864247061581 0.07411409321833815; -0.11447347572705899 -0.5560871561049769 0.0680750057792953; -0.06705788386230047 -0.46200938046607043 0.06022766091205061; -0.049086029532628715 -0.35725786450463903 0.05078115410828272; -0.04044489185865085 -0.23996050920253587 0.04039683492314978; -0.034110498545589486 -0.10823424969630317 0.03211353029920855; -0.025504423988764145 0.06607493481717405 0.015337634169998754; -0.016379042728758193 0.201103314416455 -0.001097801876741442] %
+Phase 4:
+	Planet: Saturn
+	V∞_in: [-3.7553623927693303, 3.8045661430805238, -0.0017497584909869502] km/s
+	V∞_out: [0.00016771014375336496, 0.02190103395006303, -0.00015322066785738935] km/s
+	time of flight: 2.0181733919676498e8 seconds
+	arrival date: 2038-06-30T11:10:25.053
+	thrust profile: [0.18326801514146682 0.11845670033224177 -0.0016084372043512012; 0.1675872421589649 0.14235871799128041 -0.002787329388980011; 0.14198390921850934 0.16511394888691344 -0.0037731022920933425; 0.10352323696814321 0.18228824596062612 -0.004414585252525113; 0.052724231521741716 0.18616944898352478 -0.004616750142156716; 0.0011654214657718389 0.1688827891674893 -0.004589773974233177; -0.031151502893950005 0.13429086557793365 -0.0048861485136074976; -0.0387542725070042 0.09962903031836343 -0.005697801228946161; -0.032764472688793025 0.0752213826812925 -0.006648655387876376; -0.02303421181483975 0.059664277716287864 -0.007393815905338262; -0.013366915890350172 0.04886766638458846 -0.007849749770643184; -0.004273656127481105 0.04004011769410306 -0.008128123571266301; 0.005274989439679697 0.03136991809704025 -0.008359024971909892; 0.01659789890620425 0.02034976567361285 -0.008341112112060404; 0.027347691011068397 0.0015674507187789124 -0.007372599601001636; 0.03221036017744093 -0.01353396250128953 -0.004949290348108288; 0.03641858295092107 -0.025405796803472054 -0.003362734977936097; 0.04156323966242008 -0.03555478122658915 -0.002142996490186938; 0.04760308383336786 -0.0450888885925399 -0.0011510722358481168; 0.05448090196904719 -0.0542737048917187 -0.0003050212878129177] %
+
+Mass Used: 1175.3239683910674 kg
+Launch C3: 132.40216858944106 km²/s²
+||V∞_in||: 5.345790240905041 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-13T10:50:18.877/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-04T21:45:02.327
+Launch V∞: [-5.6873787586821285, -5.786560442422183, 0.9648939525882495] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-7.006322293689667, -9.989734050925524, 1.6254097214081484] km/s
+	V∞_out: [-4.934010055766463, -9.703163112990516, 5.746968526613558] km/s
+	time of flight: 6.009580685315006e7 seconds
+	arrival date: 2026-08-01T11:01:48.327
+	thrust profile: [0.9617110897949794 -0.8739870599865779 0.8811871230841061; 0.9871206021010024 0.9481933351857079 0.8854228336153014; 0.9863523895604293 0.994327102707624 0.946716091473592; -0.9902056621813372 0.9875449005030636 0.9064066950201374; -0.9820144764851901 0.9653224112558945 -0.8337378769726054; -0.9555449311854642 0.9657521915091073 -0.8456397221554082; 0.8186521316331613 0.967179361186583 -0.8354191171549058; 0.9767230165471376 0.9633104362664976 0.8377573650125992; -0.923042165035667 0.9919872228857152 0.9072115878002239; -0.9795463340184644 0.9795259853082192 0.8043752807295302; -0.9406150428550025 0.9782073002286426 -0.8112902954782957; -0.9274513227444565 0.9828383292971064 -0.7908058073919068; -0.9533956589270561 0.9748228662065541 0.7281952198186104; 0.9661510428771182 0.9785109691567555 0.8177356035250066; -0.9664218820049025 0.9817142137862231 0.7757757339784036; -0.41334310959750825 0.9802838606130235 -0.7678896522100085; -0.45597066444496603 0.9873708363619297 -0.7744051986443704; -0.9751395557218714 0.9865324811670309 0.015824267622547083; -0.9280161403357648 -0.21108826761839836 0.6838857520556988; -0.9068916875233747 0.9712348792258906 0.6625057816879225] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [0.9553442830870951, -4.417820869496186, 0.18766425709383633] km/s
+	V∞_out: [3.7230072885828505, -2.499904853935827, 0.5960484347667763] km/s
+	time of flight: 1.0487898448288682e8 seconds
+	arrival date: 2029-11-27T08:04:52.327
+	thrust profile: [0.6774159131877868 0.6493226854927665 -0.532007553101398; 0.3302022275238012 0.6809208454980107 0.6535627201607142; 0.19857305554347673 -0.15250831748180288 0.670517038923704; 0.7186153785765315 -0.29289494991471887 -0.6203374026439823; 0.7630231141068492 0.7474131605948617 -0.34388402323483247; -0.14653416819603318 0.7578630202380595 0.6440008885838143; -0.5716565111866172 0.05476072550231505 0.5826761302304793; 0.7550937919052704 -0.5973801143592986 -0.5772563443665387; 0.8445567824974203 0.7474760718003378 -0.39238459367822853; 0.4972794197237329 0.8504015084039828 0.5954464117194335; -0.6051101474071697 0.6920479334729668 0.6384433528223871; -0.5485003210233016 -0.6848384869177934 -0.17001698436070412; 0.8818645425824932 -0.5572287228442382 -0.6059169981172697; 0.9056867468320952 0.8620079636158319 -0.21179500810720392; 0.4498657884312737 0.9206863989478159 0.626472113013419; -0.7063855626923453 0.8392260172345695 0.6657911934666387; -0.7725890297740363 -0.6321620848297606 0.35516589931735515; 0.7603264864364883 -0.8557533022845115 -0.6311629259349868; 0.9561247545973677 -0.5017701499231864 -0.6272119558821079; 0.9705083590037089 0.91129864219974 -0.2888985356409027] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [5.038952819515676, 7.9798066215675565, -0.8715896824986642] km/s
+	V∞_out: [-0.012236099214684017, -0.9981497941651291, -0.828378100790254] km/s
+	time of flight: 2.2176624458787963e8 seconds
+	arrival date: 2036-12-07T01:48:56.327
+	thrust profile: [0.9561858721260394 0.9849199946256132 0.5225438470279931; -0.027932742829215068 0.9733888937163413 0.43219740244487903; -0.44415834968745566 0.9310525799775682 0.30834923084684457; -0.41854368011913534 0.8702966170896927 0.208080577565248; -0.32933795593388565 0.815451911934079 0.1254126724065932; -0.23552180201632114 0.7723076604175301 0.06921155682993804; -0.1614904990435074 0.73600434327184 0.037191049603114215; -0.10093276866257177 0.7015622404196313 0.01739015687986595; -0.07061055518612644 0.6657821229767328 0.004884538754076532; -0.04673703754899972 0.625817515327918 -0.0025122978941227465; -0.041112337800284074 0.5793466390354832 -0.006303799076519013; -0.04283624698244216 0.5243842265930279 -0.007497163409016717; -0.05346092222703407 0.459582480493242 -0.0067340993382808785; -0.06895608005212821 0.3833475120313622 -0.004880957209105144; -0.09923125957632768 0.29425585856793157 -0.0013249599275947555; -0.13231914932868194 0.1912438331345806 0.00453604080839281; -0.15508316129336963 -0.043236971591321775 0.007944115104287169; -0.17629889261241166 -0.11291544563125626 0.012864022185234279; -0.14568672081150158 -0.25880004071832907 0.015796279090581688; -0.1516335446629711 -0.3568240854796575 0.021534187052804105] %
+
+Mass Used: 2773.596934253452 kg
+Launch C3: 66.76157923825527 km²/s²
+||V∞_in||: 9.477764916347974 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-13T15:09:50.799/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-03-26T07:12:24.150
+Launch V∞: [-4.691695981755256, 2.4100997067687473, -1.107625419239362] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-4.566977871130657, 4.760076803915006, -1.7341280162885988] km/s
+	V∞_out: [-6.208492431552701, -1.9096233111972523, -2.080047657050257] km/s
+	time of flight: 2.0717178639097057e7 seconds
+	arrival date: 2023-11-21T01:58:42.150
+	thrust profile: [-0.14461666591877725 -0.010674923527958081 0.07319622237982218; -0.2632510872185629 0.01896952413347131 -0.11219362381384182; -0.35509253776259864 0.05130847606843313 -0.1020767266141743; -0.43017679281809584 0.05045981562535008 -0.1422217250671829; -0.5045985167824136 0.01741583415172031 -0.16844373611917648; -0.569330040676884 -0.05201323466205199 -0.18486385532265195; -0.6249141520690602 -0.13905479590410533 -0.19964164942840817; -0.668271188513656 -0.2602797013356586 -0.20608604356710608; -0.6652598099366694 -0.39412254799113705 -0.19894484200845694; -0.71516785653991 -0.49228396872807745 -0.21106475073434702; -0.7140520681258179 -0.6492058751655467 -0.1932030922695093; -0.6868766770794695 -0.7396924869993249 -0.17353711242581565; -0.6152532209931442 -0.8020815173678328 -0.14764124943790446; -0.4622171233071141 -0.8398654668968106 -0.11185995276929935; -0.16854886447084155 -0.849107084555043 -0.06766821177549498; 0.23324400917872504 -0.8297560629709333 -0.01536095606168015; 0.5186243199535893 -0.769610557984718 0.03995200418629567; 0.6187570125005067 -0.6500477297841986 0.08764709560669148; 0.5808087120622782 -0.5121872212939763 0.11783856477232442; 0.4583737403324055 -0.3712720822360683 0.13462225195583247] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [-9.200127095735333, -6.894307184186653, -0.4734726391357551] km/s
+	V∞_out: [-7.90745728238742, -8.353687515473082, -0.3001668168215188] km/s
+	time of flight: 5.676487860450122e7 seconds
+	arrival date: 2025-09-08T02:00:00.150
+	thrust profile: [0.9450818166379835 -0.39326487285299566 0.08478396733763034; 0.5033926889693318 -0.49600851782195465 -0.09864181576764529; 0.593874568813462 -0.5134648071397765 -0.21563608217734162; 0.6726275954838512 -0.44694734612516734 -0.3151164039729524; 0.6947676879446373 -0.29388960390973834 -0.3690682632127033; 0.7117640920103931 0.07243876441940703 -0.41029659430010107; 0.7001034602049846 0.6195031306652655 -0.4186969404202771; 0.695103119957999 0.6808867140504492 -0.4033934445136916; 0.6468162520522805 0.7276709960247509 -0.3673200063653498; 0.5786083720048963 0.7618030225293763 -0.2740863676479381; 0.43998280657362615 0.7813682905260836 -0.09859638125917183; -0.04546726863354173 0.7884156184890568 0.05317843281930274; -0.6546093330399981 0.7727091843423107 0.11218174811377148; -0.7965171690457952 0.7496124509846286 0.19970259425421277; -0.8736983626104139 0.6200392713895918 0.2654841797347523; -0.9103125128246278 -0.6456308917849752 0.27992773703210205; -0.9019970750226028 -0.9023670767015256 0.1864233187998923; -0.6771646049748614 -0.9414644139448815 0.011110810182933379; 0.3521154040459276 -0.9440844390692263 -0.16519285405497774; 0.7774895055238358 -0.9371489950391606 -0.2516063758929405] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [5.616813665429002, 6.787110157183047, 1.2069938406439464] km/s
+	V∞_out: [2.1970387730495697, 3.225023288265242, 4.175802839196012] km/s
+	time of flight: 1.6257487956751725e8 seconds
+	arrival date: 2030-11-02T17:41:19.150
+	thrust profile: [0.9505134233163771 -0.979494400300436 -0.30984147298673975; 0.9511180319113616 -0.9647970604644283 -0.6501969016781382; 0.9424633459203795 -0.9926658842113464 -0.6207418959532092; 0.9304882859838348 0.23850084565208374 -0.5933249374851602; 0.9098194053379338 0.5493464195536784 -0.5111960642202787; 0.8829443918138722 0.6659627102171121 -0.3774953044827189; 0.8472666578022966 0.7031440366152961 -0.2698632635749556; 0.8051838923072202 0.7113118353482547 -0.23246846453046197; 0.7503491889394095 0.7106325372593361 -0.03813921871732603; 0.6848270191956657 0.702152969321232 0.03334922254887817; 0.6172988381336922 0.6882916490356381 0.08048503574576253; 0.5480320293122681 0.6685098976431961 0.10512250251977935; 0.4755966950131009 0.636871879957033 0.11757167935113788; 0.3912388892675421 0.5870441077418865 0.12131662398055057; 0.3071016125028102 0.5153387959524959 0.11568557231704885; 0.2061494535664333 0.42029155244133604 0.10481292164087117; 0.14105224096703986 0.31043414548479376 0.09141235006535123; 0.04128524414299072 0.18984755798020106 0.07349121047003337; 0.015873438623124358 0.05896310201745711 0.05559998369192176; -0.03554622243905677 -0.04901685480247809 0.04100049118737373] %
+
+Mass Used: 1688.2891346811068 kg
+Launch C3: 29.04742585113039 km²/s²
+||V∞_in||: 8.892147894026486 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-13T17:44:34.669/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-01-06T04:29:48.093
+Launch V∞: [0.5457290374235895, 4.341334791096552, -0.7559687755701914] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [0.8335159107192338, 6.90456105315263, 3.5067701274587337] km/s
+	V∞_out: [6.76973645767487, 3.7624182770964607, 0.8285997001531188] km/s
+	time of flight: 1.0236386879690988e8 seconds
+	arrival date: 2027-04-04T22:54:16.093
+	thrust profile: [0.20124636719972494 0.28871460999851783 -0.24826466053632043; 0.21757301989581354 0.24241685861764573 -0.2950961505210993; 0.271442849091815 0.07872734315816171 -0.19097989520692127; 0.1879742866678929 0.27655633192716367 0.10042573300235896; -0.14244608091005748 0.33201061328346854 0.19340046097242167; 0.17387986662182686 0.3014608753850556 -0.15431719711609648; 0.18777345028680853 0.2673897380502672 -0.25525617202163087; 0.2556315993639935 0.17739994769888612 -0.27159167007539076; 0.26609722508102157 0.2783459216563457 0.051977998587726774; 0.0438700045849084 0.37141025221234536 0.20109295136087044; 0.06232447288714108 0.35663405987308516 0.024990128722474907; 0.026521151688839967 0.3160983251683631 -0.16548739972882243; 0.19612956542640614 0.24782370475857005 -0.2471047602651378; 0.31651280507021246 0.18621565754181835 -0.19804312266917037; 0.24435157836852087 0.3468639663937176 0.1852596358565247; -0.00965870127546034 0.3979396968294011 0.22213565307438407; 0.023169341463938578 0.30016276019204574 -0.18664622656660942; 0.1268886531461076 0.20680899035126646 -0.25936562207083624; 0.2125169373278653 0.24319285890159614 -0.22236991044858823; 0.35244171182303646 0.25085960304558635 -0.1638088094827891] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [8.963228181916202, 3.147920284899006, -0.7449749580149643] km/s
+	V∞_out: [9.377239868662178, 1.0270817933951877, -1.3450268054813155] km/s
+	time of flight: 1.22946548225175e8 seconds
+	arrival date: 2031-02-25T22:43:24.093
+	thrust profile: [0.2815247284876436 0.4687108668970388 0.07024363175566978; -0.28575122080824394 0.3851477052454153 0.016801525539966562; -0.3747967738284827 0.29808121010819033 -0.07185502866615309; -0.442929227216859 0.19222627634169495 -0.135743553778548; -0.4487478745447117 0.1327038699880746 -0.09503248552633654; -0.49852432866134694 -0.13114566918915876 0.14249733878062454; -0.4800686097933296 -0.20421918036330872 -0.007593654428925882; -0.29831925246774027 -0.05272129811015332 -0.01656649869964936; 0.035964682967361335 -0.09683145552380305 -0.15527299210182244; -0.09302182221116087 -0.33887428309830736 -0.2404084153476241; 0.5923912702376002 -0.02542163181573757 0.2009826493089844; -0.02623028033428319 0.13880579512402433 0.24850570533865052; 0.29039130962158227 0.3062352881282009 0.1527335375754828; -0.12082271353315516 0.4096496613048553 0.02796560796386028; -0.027194067272572214 0.35743634565580396 -0.04064730736657738; 0.04127166490432071 0.24768556235295525 0.09118781754436289; -0.11854966698415786 0.22553475056440592 0.08555412347860751; -0.1806405003127596 0.10096300132551984 -0.15472306505086783; -0.20075020241889296 -0.009061662245205257 -0.11023054116740935; -0.2987954790790834 -0.230652241463122 -0.11725959697110766] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-3.1812528488033522, 8.51185716671171, -0.7460758734937367] km/s
+	V∞_out: [-0.21505538492794815, 6.349830695161589, -0.12985627371130587] km/s
+	time of flight: 1.315250993552624e8 seconds
+	arrival date: 2035-04-28T05:28:23.093
+	thrust profile: [0.7987730439865184 -0.41345767452772897 0.001505324112112355; 0.8674728852573501 0.6602259691893515 -0.0759345729834176; 0.7597133759248544 0.8594908841609692 -0.19125255627342094; 0.2872093106917861 0.8668264267695036 -0.18904379386155162; -0.5401943922623963 0.8498080030613695 -0.16437663889563423; -0.6896408194237241 0.8199272255247071 -0.15201175224165175; -0.7134753635114731 0.7870386683779858 -0.14239308646192794; -0.7170346050334127 0.7501463142097656 -0.13294598405115826; -0.7002315120575128 0.7090750008587086 -0.12315905659225605; -0.6872097378697336 0.6676696143275933 -0.11572226052465101; -0.6627939184703779 0.6168905813867107 -0.10527146741337202; -0.633554979686539 0.5685903428331747 -0.09336745543158023; -0.5918530549537074 0.508122677783068 -0.07972015422869783; -0.5468540100379315 0.43929599357406623 -0.06477133727408631; -0.48985935766804956 0.3608169402041227 -0.04832795620510983; -0.42117899759427235 0.2697982895066768 -0.030347981218191687; -0.3351818344708077 0.16466291198509436 -0.01189485088684984; -0.23232691164467884 0.0500315224688059 0.00787577036146254; -0.1131949765395752 -0.06833292217756129 0.02847742053557143; 0.005991615157979781 -0.182291757352861 0.05024929371428449] %
+
+Mass Used: 1536.01990119313 kg
+Launch C3: 19.71649674030971 km²/s²
+||V∞_in||: 9.117494794269444 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-13T21:46:30.548/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-14T22:50:54.151
+Launch V∞: [1.1286314645978788, 6.894494804991318, -0.8285243221011761] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-0.4975358362817743, 7.143314145080825, 1.4331811045093779] km/s
+	V∞_out: [6.0255649206667625, 4.05582288696785, 0.7567303017536462] km/s
+	time of flight: 5.201873526429285e7 seconds
+	arrival date: 2026-01-07T00:29:49.151
+	thrust profile: [-0.13658867986140374 -0.24246001363888786 -0.0018351721366561648; -0.19874653605027093 -0.42347951183192895 0.059887224602709746; -0.006030933718274198 -0.6165659086877646 0.05143110252875157; 0.5690891294297716 -0.6337278673409295 -0.012184805314118167; 0.6969370055919233 -0.3303175586786053 -0.07217788171252011; 0.64128971249768 0.26314536468162564 -0.09952967531295756; 0.5208719713422499 0.32770505919622234 -0.10513933945114934; 0.4271266849981205 0.20190088190483316 -0.10365532774681949; 0.4176630482221774 -0.011898915901332388 -0.08241345687785652; 0.47262980673060484 -0.13896143178119608 -0.03374381004058062; 0.4421659456699236 -0.17124612763461697 0.02403617877878262; 0.3583106766681072 -0.28808344084851756 0.06553065121634129; 0.4748177430173668 -0.46986296014010215 0.04039987329214622; 0.5807725097378242 -0.2734128860609197 -0.035376229041435836; 0.5547393823521555 0.03932247507743895 -0.09732884535240749; 0.4576988071163949 0.017725627686673677 -0.1304971469405435; 0.40441128328564385 -0.22624714092575637 -0.12589052393340233; 0.5227891982702978 -0.37951138376215193 -0.08197543798043004; 0.6869211599682585 -0.3895945340441026 -0.04215815195764137; 0.6943636261137554 -0.06601804604492464 0.0018331949690765612] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [6.338828850719935, 0.2060782119786431, -0.4977472310639235] km/s
+	V∞_out: [5.762367354839256, -2.687069620550792, -0.2168349056959969] km/s
+	time of flight: 3.949974283472407e7 seconds
+	arrival date: 2027-04-09T04:38:51.151
+	thrust profile: [0.458336717149733 0.1771870373806907 0.056427191918473445; 0.403817033597994 0.351117374215139 0.15075644725276122; 0.048711917893504396 0.41093296017258263 0.16380972666043295; -0.18354926599538152 0.4256482504531366 0.15401233744770568; -0.42370527996013474 0.23794979462159155 0.1314849420842794; -0.5679456579714863 0.1393409941124382 0.09924531892954472; -0.6520211065270787 0.025161300456823018 0.0635649864433606; -0.6989667221671542 -0.10489669213488008 0.0253021698618907; -0.7262214288474695 -0.24555410262257685 -0.0121562278547937; -0.743313608223649 -0.384644672098393 -0.05649462601447925; -0.7525404848639327 -0.507291521547137 -0.08734741229955949; -0.7578561155541664 -0.5996752434898261 -0.12360313032488564; -0.7592183352851313 -0.665338122647058 -0.15810104649178947; -0.7558073245676104 -0.7094328622253643 -0.19027889839324838; -0.7464517819119382 -0.7464555301053758 -0.21801144025375926; -0.7296456019615701 -0.7634101584430326 -0.24323055639952082; -0.7009447676318107 -0.7794725581151669 -0.262851486143965; -0.6543199308894584 -0.7903707443682346 -0.2772415958605197; -0.5827848217677881 -0.8004854095656452 -0.28523650701311554; -0.4849301355226277 -0.8048943851748858 -0.28659470269055276] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [4.322617308702803, 2.354348521583675, -0.7376335957485771] km/s
+	V∞_out: [3.011554362103189, -2.0958590497922804, -2.908427301510971] km/s
+	time of flight: 1.8820349650227648e8 seconds
+	arrival date: 2033-03-26T11:23:47.151
+	thrust profile: [0.9368347194497842 -0.965371940721398 -0.5613882989973752; 0.9714384488821548 -0.7607872705031594 -0.09024131587466705; 0.9505668891632969 0.8312812365923358 0.07095989545704967; 0.8695060114456342 0.8325193176250749 0.07116267827484891; 0.6939833190653248 0.8028129129322639 0.031577569215995506; 0.49217044040756264 0.7963553158741095 -0.021466953451174452; 0.3421171062041329 0.6993381181757932 -0.06563494914488495; 0.24925579641473375 0.4813067954039389 -0.1267909830819491; 0.19205090715099823 0.2932984515362608 -0.11766481272251779; 0.15209938030796544 0.1642850960501914 -0.12314405675789696; 0.11581486470625263 0.09373283562323559 -0.12395161654174959; 0.08005933539569969 0.07505479185768685 -0.11065807756901873; 0.04290428379494743 0.06421252941862582 -0.09362719990942882; 0.009670159523961858 0.05833849578599656 -0.07211230161173374; -0.05839187604989335 0.06373138672808198 -0.06233551857721689; -0.012522824962244553 0.049309431568300005 -0.040752415650939504; -0.04320895480635503 0.05485848479687612 0.0021594467585038988; -0.03809749205187863 0.0378883881221725 0.04099809276024048; -0.035012269320380346 -0.006618884738808792 0.05971979961122836; -0.03288959167972974 -0.001403295597270634 0.07024375436873588] %
+
+Mass Used: 1258.284359858289 kg
+Launch C3: 49.49432015124584 km²/s²
+||V∞_in||: 4.977155882645959 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-14T01:43:41.263/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-20T09:06:35.288
+Launch V∞: [-1.8438889475809765, 6.120059172103301, -0.7981747861634966] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-2.56509812262509, 8.726298030365955, 1.2653783448963722] km/s
+	V∞_out: [3.933875520715713, 8.182318027927845, 1.3797206772984685] km/s
+	time of flight: 6.3150638478290446e7 seconds
+	arrival date: 2025-05-20T06:57:13.288
+	thrust profile: [-0.1673002601441919 -0.26883139314945603 -0.004056802930588146; -0.23150973398793398 -0.5422926057887579 -0.01424916584017891; 0.5216279513936498 -0.7201035092402946 -0.05026572450882597; 0.7619564949501179 -0.017659100038672788 -0.050798263624736634; 0.5942837250609073 0.5263617574161898 -0.0070195713227723154; 0.3410765842139262 0.41102934542119196 0.0003621379767194054; 0.23648394719297353 0.14198690462048363 -0.009581961375511473; 0.0056202015516126 -0.32693032741518907 -0.010162609157081665; -0.026379909967065362 -0.5874916310490459 -0.021494316985701284; 0.693629555909135 -0.61456318000757 -0.054644453501477036; 0.6749160281202036 0.3944492779701146 -0.021084849056050275; 0.4403512073946586 0.404989286932993 -0.0014708947868851455; 0.3219167787670785 0.1274096536884702 -0.008385265303928385; 0.27124921840307187 -0.19763134120286302 -0.014529551099335972; 0.08063379563374638 -0.44308484663335224 -0.017300342160510865; 0.5868779992877718 -0.6080198456071109 -0.04284179805368043; 0.6638767318711757 0.23800863124179605 -0.023418413571253783; 0.44792722794577955 0.3189162484584814 -0.0034061188086769605; 0.3654940275210002 -0.01822248382616463 -0.011103744313695233; 0.3671390691769647 -0.1877557855665406 -0.017972667398621946] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [3.740909417528976, 4.969698645681673, -0.1836371554650627] km/s
+	V∞_out: [1.6805078934236426, 5.988466382534255, 0.2011389183183449] km/s
+	time of flight: 9.967373816267239e7 seconds
+	arrival date: 2028-07-16T22:06:11.288
+	thrust profile: [0.2889046493274145 0.35172813894699617 0.005750881627058749; -0.2891211816810922 0.2856217397496342 -0.01070529954797825; -0.4076909207469804 -0.04788044763953207 -0.020561543485485726; -0.37899315325138216 -0.30969571658846323 -0.020466381356948952; -0.27651505042097296 -0.43501262129876456 -0.018271754879646666; -0.03992270374633847 -0.4908301495597925 -0.014401728962937026; 0.28778598754683493 -0.4545602376768821 -0.0064508479743784625; 0.46150433893131715 -0.1880814631199537 0.0021626109204597446; 0.2788204255677078 0.360854942969168 0.006831262006997803; -0.2566515872209155 0.32209934564164727 -0.007836893916662625; -0.4100446444003415 0.054443015280224105 -0.01751477422173226; -0.41902900656224723 -0.23975107675376675 -0.019442357179398642; -0.3644374200145407 -0.4010601518340647 -0.01891998107003531; -0.23193420972805218 -0.48910794102085664 -0.01726021542869752; 0.04132505041766476 -0.5223896099070574 -0.013713715632566187; 0.3300017630006415 -0.4784824951035753 -0.008331679149800309; 0.48040380368063845 -0.26935494128032167 -0.0016253936871342854; 0.4263256047487922 0.26594823500945197 0.005887216845594874; 0.028855636881693788 0.40742654653958477 0.004203409756847152; -0.30902036281985135 0.2999387343974258 -0.004381705457322128] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.2399121705505638, 6.956855519313853, -0.5166911303842717] km/s
+	V∞_out: [-0.00013639678575079212, 0.00045388258983991705, 0.00010352289927939363] km/s
+	time of flight: 2.156567539242905e8 seconds
+	arrival date: 2035-05-17T22:45:24.288
+	thrust profile: [-0.5883389325549248 0.34393534356111716 -0.04223302913356034; -0.5094157452497227 -0.32578128865408745 -0.0418290876544073; -0.2837278960528077 -0.5200051898159135 -0.015714467863770183; 0.234663577149613 -0.5778749576697557 0.007285867554073748; 0.5269009945794882 -0.5533424499427229 0.029448586498405305; 0.6588494889448501 -0.42596433225988556 0.03990667436449693; 0.7104940582670465 0.09976028717408182 0.04288674512400733; 0.6731412653152242 0.5520777962943062 0.03383456434541915; 0.5144161575829512 0.6548774334195933 0.016436082603795563; 0.18808395700108824 0.6460817168459387 -0.006174956813691272; -0.08944132984324173 0.5852109928553235 -0.02412032985192145; -0.1777044504999653 0.5026107885439219 -0.0332038631526247; -0.18602955062431278 0.4183028818306649 -0.035496117853459554; -0.16885700381769508 0.33802299933222757 -0.033691289488692565; -0.14420336819801963 0.2608351709154188 -0.029504852011938868; -0.11794830800737324 0.1841852103036704 -0.02391639449132369; -0.09183314607853647 0.1059536639685903 -0.017483392600732773; -0.06633021176691514 0.02374701364948183 -0.010504070567046215; -0.035138504389099774 -0.06203575677661479 -0.0031448184775343894; -0.004807991844724756 -0.13909256410647852 0.004015212913470968] %
+
+Mass Used: 1533.705930555565 kg
+Launch C3: 41.49213371032417 km²/s²
+||V∞_in||: 7.085350424044305 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-14T07:13:59.762/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-02-16T05:05:32.419
+Launch V∞: [3.453247666372975, 3.054378572063566, 0.6410592621774811] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [4.153079961936853, 5.459670821339341, 1.7440959409843952] km/s
+	V∞_out: [6.710988704381646, 0.6372991451166926, 2.1574305475746165] km/s
+	time of flight: 6.880360130276513e7 seconds
+	arrival date: 2025-04-22T13:12:13.419
+	thrust profile: [-0.16468330421268426 0.2189329295052185 -0.010873373523340836; -0.37786012024771315 0.20083778181188183 -0.006424325713147286; -0.5363839840515389 -0.21650601709151382 0.008355901825288066; -0.1834968949564447 -0.5561458893436484 0.022693080099818807; 0.25056844492648533 -0.3743357803658322 0.01765926371738561; 0.1740788365495075 -0.23152478296259496 0.027396199892226875; -0.2272240445300924 -0.12216723581853697 0.0019073418117069496; -0.30400700667720765 0.03385256284712383 -0.0074809413195897415; -0.4432437436533131 -0.12491757205634534 0.001436858833454895; -0.25527810292667125 -0.47170642997472956 0.01723278603053477; 0.10898711472363787 -0.35128780086659317 0.02104164145167786; -0.12804417889558464 -0.30272123758944086 0.0327809201214705; -0.18015320445436095 -0.3135806255343057 0.013653240243077786; -0.2094636680250507 -0.23126228233960147 -0.011785210455459378; -0.33027685949511737 -0.16914499178629147 -0.004386004892518824; -0.20190263120461807 -0.36731341845462673 0.011628082895590211; -0.1902112001660596 -0.2648905855353262 0.025952835297502176; -0.31508347575033296 -0.29163705829609193 0.023397543761390662; -0.20963477326342633 -0.39341238177599347 0.016402862738082804; 0.002812966706787112 -0.3622400996934989 -0.0021344748372502283] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [7.040278950309005, -0.7501648907703503, -1.1912371523753373] km/s
+	V∞_out: [6.888311168909946, 1.6990426218863528, -1.100876807493356] km/s
+	time of flight: 9.342629092297508e7 seconds
+	arrival date: 2028-04-07T20:57:03.419
+	thrust profile: [0.356740070161183 0.09173310552676897 0.016574996568492047; 0.19378678269157593 0.4003618878297842 0.0381127321481018; -0.14928159447866768 0.4268446644300027 0.0715397377621758; -0.36113057153024997 0.33270767280174496 0.0696644041484723; -0.40841967844319355 0.20314247070355662 0.06584645395451007; -0.3961511181475026 0.051309814044093315 0.0613267572370165; -0.26862361927193956 0.025846072419724607 -0.008417903267850992; -0.13635376645426722 -0.285269600012018 -0.08480671134086627; 0.48172274225702855 0.03908288821073942 -0.05302198385151616; 0.29736513890266103 0.49380435392567307 0.005932551117785213; -0.1985367964283465 0.530870057786597 0.0443930796666557; -0.42331702745207156 0.43958981624872456 0.059782969970213436; -0.5008191025029283 0.2545821318245874 0.06513111946463424; -0.5090995507101782 -0.08132366596204624 0.05557971290084116; -0.4365235221818152 -0.3526326460862695 0.02944186352246856; -0.2428244049915453 -0.47913502242306927 -0.001429975852898112; 0.2965174674673905 -0.4998400318898462 -0.025394379226107915; 0.5581409602767857 -0.2670720924249945 -0.039037417950486986; 0.5404240598856603 0.4588278322563326 -0.025739054026010875; 0.26481365444928556 0.5889586368264279 0.004310453551953653] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.768248852275849, 8.741237951612776, -0.10565185114199886] km/s
+	V∞_out: [-0.5689195906105274, -1.1835291484022944e-5, -0.00015076538393807672] km/s
+	time of flight: 2.0647184294271883e8 seconds
+	arrival date: 2034-10-23T14:14:25.419
+	thrust profile: [-0.4118350568502539 0.7397165160046664 0.03650850663151651; -0.5341616982673818 0.5894274810704492 0.048162894586397755; -0.4755846337249282 0.43205141226513055 0.041845478429139625; -0.39146679855903316 0.2793885116422214 0.02666641123567999; -0.29760210470836107 0.10001617063364038 0.005246077036260758; -0.12498798746952003 -0.08547038452801747 -0.03186649737115955; 0.6012927333188255 -0.45651427473844913 -0.006324492609029606; 0.7279077782996053 -0.47845321826514736 -0.032106373666422404; 0.7991128821218656 -0.008283851491542838 -0.07299734954029101; 0.7175587921889662 0.7765717901964799 -0.0800061252435837; 0.3713835047173401 0.773068311463042 -0.038433384532840224; -0.22213951903671245 0.7320154781062939 -6.0672070416028177e-5; -0.3604362859233379 0.6654377220105319 0.014630889316898951; -0.36946080731663716 0.5882623820858978 0.019090223705502275; -0.34750278679765795 0.49839847471976123 0.019927901000876793; -0.31336540870223417 0.3875868492542638 0.019145167045154086; -0.275163205347443 0.2458793980758599 0.017720554190660976; -0.22860840531216062 0.04253129834335439 0.015609619947715278; -0.1634843649420853 -0.13471729070541885 0.012551273723230135; -0.0964949439134174 -0.2770815913878259 0.009813568018480465] %
+
+Mass Used: 1584.5276313627078 kg
+Launch C3: 21.665104884415 km²/s²
+||V∞_in||: 8.918918501922759 km/s
@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EVMS_2021-12-14T16:31:21.927/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-07-04T03:26:06.312
+Launch V∞: [1.0595449194495574, -5.179046997413335, -0.710854272622436] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [0.7167821480418011, -5.3523238156588455, 1.2976343649115025] km/s
+	V∞_out: [4.57208952781187, -2.763307224201735, 1.5182287145267939] km/s
+	time of flight: 5.770490213360378e7 seconds
+	arrival date: 2025-05-02T00:34:28.312
+	thrust profile: [-0.012518442262623266 -0.2846133058802652 0.036714163181811914; 0.04598892978893719 -0.4496628555421884 0.050821562545283167; 0.23858170610390916 -0.5534890194603386 0.053378611889742245; 0.45971698047001736 -0.6075384006689931 0.049225674552565796; 0.6103599468173085 -0.5939492998556735 0.02390794631734322; 0.48631512404956767 -0.5016073617028688 -0.0035970332832769504; 0.7205092838499264 -0.06817749918391544 -0.030568869866240404; 0.6554236549877296 0.43397088287936925 -0.04092445445978924; 0.4426214422172243 0.5233653736000612 -0.04291086849556375; 0.1265987354418195 0.37111271167996557 -0.04211705533923255; 0.14291026132925347 0.10951608658101342 -0.03253146989706353; 0.043819468335856315 -0.2760884262553685 0.027757067112302112; 0.12296287504557858 -0.4824942105922541 0.039565941973149145; 0.34178968176729657 -0.5570754798887297 0.042557000779956305; 0.525918072341391 -0.5414835388569836 0.028260866562936558; 0.6470594344300419 -0.5105003019983401 0.0030006706220706667; 0.5771986338738871 -0.2149560721661336 -0.021449899364102736; 0.6724367414193944 0.3342772748116172 -0.034581763000182654; 0.4545022153210568 0.4845067333568687 -0.03498154387686175; 0.15460631758712481 0.30947276279006714 -0.034528617189168165] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [6.053679269318452, -2.70754196571206, -0.561868816241759] km/s
+	V∞_out: [6.62831028724014, -0.0335448848261144, -0.598213998623492] km/s
+	time of flight: 9.066465712235557e7 seconds
+	arrival date: 2028-03-16T09:12:05.312
+	thrust profile: [-0.14077705817283215 0.17219038983580243 0.0010673207963448805; -0.09076911485954396 0.3656127875299659 0.07959031496882961; -0.22901583771408088 0.3398208518705999 0.1109715317716953; -0.32670071352071345 0.2280441403604959 0.1147286298393803; -0.628253671808909 0.07416681520769915 0.07809920940474491; -0.3363546214364444 -0.0738216870465495 0.051587092016739784; -0.22220741723836346 -0.1904607293157175 -0.008841671167926259; -0.032348160495606626 -0.20217939877808486 -0.09753767695663382; 0.29315934163115015 0.09200142472327252 -0.05343148185045425; 0.24059656978259783 0.37859909374997347 0.022698241631866987; -0.0271078201127222 0.4659834877302928 0.08034951421535458; -0.3164477633221403 0.42340838072348136 0.106820004124928; -0.4327826247755731 0.29532199369082585 0.10616547737632574; -0.46971892563271284 0.07217513538995383 0.07291051527360017; -0.4205532859364489 -0.17888301219299818 0.049620946374109944; -0.31397875164405536 -0.3499883855343491 -0.01722453765780476; 0.055748170553023536 -0.4155273836848591 -0.05564285735614245; 0.4306072283821911 -0.1907071754065535 -0.06468622506578485; 0.46309518107140285 0.3221076719593664 -0.026634119992690917; 0.2485211129542623 0.5082032846330088 0.04664261897154823] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-0.15931607365900702, 6.659982567616171, -0.7147859007662032] km/s
+	V∞_out: [-0.03141285197558282, 0.00666134026526007, -5.85929449610048] km/s
+	time of flight: 2.264417121463342e8 seconds
+	arrival date: 2035-05-20T05:40:37.312
+	thrust profile: [-0.3528081960729175 0.5957253626842559 -0.04112855090660253; -0.4498696875407646 0.3599016941813443 -0.008926830351384682; -0.4296518057984319 -0.20738905197149196 0.009333332557682678; -0.14954953849570887 -0.3435796518536134 0.035875098563252904; 0.39678430953935184 -0.5168745604329268 0.02935112983491381; 0.571454084996011 -0.46813508275649046 0.012118057152003993; 0.7040073430650443 0.38813276418344744 -0.0015818210549435883; 0.6929710132849697 0.6613684228669995 0.041556415408789134; 0.47766142600053263 0.7290623000841082 0.057207252732303655; -0.20126978731123335 0.6865609825371612 0.04700537721488603; -0.1726478786848928 0.5473873161459025 0.033978777160795566; -0.23702248937731904 0.5103684148600998 0.011996785197593873; -0.25066827594702035 0.42611462142301987 -0.006783200240873317; -0.19809970132181848 0.42158636663551524 -0.01768186691013301; -0.1581469693984499 0.3721724862460802 -0.026688684037946272; -0.11314582650191973 0.3541426305930295 -0.030452326114901382; -0.08143085687847508 0.2759935128733878 -0.043735992358310494; -0.025930504510641876 0.18682783519552412 -0.06228985999553243; -0.01540965514296248 0.09256748216309786 -0.0716228215794782; 0.0639416491137141 -0.15066247627007892 -0.10320894780723987] %
+
+Mass Used: 1536.9108057812873 kg
+Launch C3: 28.450477034653016 km²/s²
+||V∞_in||: 6.700124498560573 km/s
@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EVVJS_2021-12-18T17:53:58.867/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-06-24T03:41:10.468
+Launch V∞: [-2.5086977090763227, -5.909009701214558, -3.6145624632193294] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-8.641740181450986, -2.7358765971708188, 5.979083178622357] km/s
+	V∞_out: [-8.782585218349974, -2.7633891948741853, 5.757128066064576] km/s
+	time of flight: 1.3058425505068028e8 seconds
+	arrival date: 2028-08-13T13:05:25.468
+	thrust profile: [-0.7066166088184461 0.694440248124216 0.7479354980537709; -0.6327447429640423 -0.8354350485844262 0.7834527345864157; 0.9020568747016394 0.8877052626244303 -0.6463263227561554; -0.7301431150683071 0.6609966418814177 -0.7438889151598259; 0.730852451440183 -0.7320972842184537 0.7604738505723868; 0.7972709043563252 0.721855932933707 0.7718028396811908; -0.8037412340829777 0.8087516989811351 -0.7172943955497878; 0.7648238186384819 0.6552635836307407 -0.721155847669259; 0.7291150156338002 0.748678684325491 0.7866560258556328; -0.7570680522417093 0.7690073045139784 -0.6461755325555683; -0.6468702385091074 -0.8148737116229223 -0.7704229798858344; -0.4993264506198249 0.7454968352904051 0.7338556974594883; 0.7368764981991002 -0.6117948959055127 0.8068497932656402; -0.7962857723296427 0.7491959753561124 -0.654565239742625; -0.7127612827380243 0.6906152690232072 -0.77926816829975; -0.6834549942628344 -0.7126511442816399 0.7270169479529096; 0.6623991589464917 -0.6788349696325189 0.817241726963756; 0.7045461026526441 0.6832122117875238 -0.6923017984092904; -0.7118848172229095 0.6940290158932474 -0.7555659392711116; -0.6684106313303576 -0.695492267513801 0.7927961883463502] %
+Phase 2:
+	Planet: Venus
+	V∞_in: [-7.955987785349071, -1.7429230646850489, 7.048560055803307] km/s
+	V∞_out: [-8.38468808776243, 4.638807911180807, 4.920220822386981] km/s
+	time of flight: 3.903384248532212e7 seconds
+	arrival date: 2029-11-08T07:49:27.468
+	thrust profile: [0.35184470451251054 -0.3489438480396312 0.22003829255796042; 0.5775112094730798 0.3466350775731712 0.10768869846318309; 0.5151690947404881 0.6922646119099484 -0.2079306947550997; 0.03820729926768738 0.7645099364102405 -0.003934023466790116; -0.5310966588437559 0.6960577720418427 -0.2806379441488921; -0.4888319757324884 0.6421514470556614 -0.3174191597815846; -0.34372723910767994 0.6560895563596227 -0.16929444361647178; -0.3645888618705135 0.634917562387229 0.1666892583656993; -0.3850511801341504 0.7324174772643002 0.5376102954603407; -0.6275951088762817 0.7623544346482719 0.6418628750791122; -0.7919929569477481 0.5902287990856233 0.45549206134198506; -0.793859142829226 -0.27621743364089885 -0.03426934297306585; -0.6072979328607674 -0.6138362647581398 -0.4816955133844994; 0.13432682697115447 -0.5431982957931105 -0.6262239404967714; 0.5688082709851283 -0.21021884608354516 -0.5260160342268195; 0.6818162423845489 0.5160256516002725 -0.4092906774489981; 0.7130018091756617 0.7341633847919329 -0.15724287718021424; 0.6616897627009751 0.8195554298912001 0.3135759308050811; 0.1872587594296505 0.8726717894768014 0.6224150121537937; -0.6414995880519144 0.8901062055995407 0.7300574454135067] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [3.616389218491424, -5.528555297073314, 2.6454669550732093] km/s
+	V∞_out: [-4.714476188428925, 3.7327085648268112, 3.805565087766136] km/s
+	time of flight: 1.0083979624306786e8 seconds
+	arrival date: 2033-01-18T10:52:43.468
+	thrust profile: [-0.9659103696906655 0.9517515910607882 0.8168373781737548; -0.9561283643434136 -0.8761699655545768 -0.1939995320784213; -0.9275867912262411 -0.9136864536027992 -0.4060037610832777; -0.8853757072400111 -0.9132743466476493 -0.3994899790867979; -0.8271257223116684 -0.9063668321809316 -0.341644963512146; -0.7251990654980359 -0.8962396229655277 -0.2630714822249463; 0.18838507258195641 -0.8860877807707359 -0.15307132464698348; 0.6622301460691353 -0.8684657561454765 0.07422800726056446; 0.6152410169116248 -0.8481784036097828 0.2658920782241131; 0.6215425470318906 -0.8230726802555173 0.32667501700810464; 0.6389070189564778 -0.7921065374330535 0.34021110523295184; 0.6318769085000678 -0.7547402247270236 0.3362004802720032; 0.616705490069356 -0.708911815572844 0.32003622824074046; 0.5945544151167129 -0.6524425628293116 0.29334179519703246; 0.5663787104667805 -0.5830242242373314 0.2574479200400718; 0.5347064309525714 -0.49844216424182536 0.2142037683145213; 0.4986839302662462 -0.39909400732377337 0.16566817479325446; 0.45286850381956695 -0.28918436173239803 0.1141785086594864; 0.37710967383789334 -0.1678572767236383 0.06149121277195424; 0.25394438978570527 0.02043569238203405 0.009191155783547409] %
+Phase 4:
+	Planet: Saturn
+	V∞_in: [-3.2880012796332987, 2.1211606572569277, 0.48142650562617806] km/s
+	V∞_out: [-8.731880472477191e-6, 9.666612310001054e-6, -6.225039409550941e-7] km/s
+	time of flight: 2.1161982067082927e8 seconds
+	arrival date: 2039-10-03T18:09:43.468
+	thrust profile: [0.022423037123395814 0.08059850157352823 -0.1327356604236625; 0.01554844506706407 0.07575167965809157 -0.08215431382545887; 0.004436644366473565 0.0665844137373235 -0.028828351796870644; -0.008131707121939417 0.055075456865770506 0.017731675612583327; -0.02018941938325407 0.045096951581116415 0.06687637224142223; -0.02543873854159729 0.02905260962667718 0.11099986430188423; -0.022683647304998084 0.014600108269522964 0.14240131923790691; -0.01635725372584873 0.005199870254546869 0.1603574566237192; -0.009646680596205824 -0.0005145097922692435 0.16718880257957977; -0.0034057298966922184 -0.0044319774679023915 0.16564089244298724; 0.0024575970566733775 -0.007624658692633722 0.15799198592156033; 0.008185905684027191 -0.010539011665542544 0.14597553943022623; 0.013987314799160704 -0.013330717852839631 0.13093216092661572; 0.020037882876062143 -0.01605336859123858 0.11391525190686709; 0.02646489450515348 -0.018721137962794496 0.09575475738764945; 0.033373123348953045 -0.021357123294403972 0.07717404261022846; 0.04100633524272448 -0.02409647883011826 0.05884172751529372; 0.04996375895080879 -0.02726627285470597 0.041127114982092414; 0.061081932228138576 -0.031206207742307278 0.02360571733260185; 0.07466681359328371 -0.03585261547468276 0.005215821732814806] %
+
+Mass Used: 2591.3951917643953 kg
+Launch C3: 54.27502164508673 km²/s²
+||V∞_in||: 3.9423402223912998 km/s
@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EVVJS_2021-12-20T15:47:12.591/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-05-08T02:15:41.742
+Launch V∞: [-2.6705377464328075, 1.81220401477148, -5.02986389717478] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [-2.6649059053371618, 1.1318437761748215, 5.5271509852418275] km/s
+	V∞_out: [1.5500163131788576, 3.701161902600424, 4.7781830264083816] km/s
+	time of flight: 1.2506637578161152e7 seconds
+	arrival date: 2023-09-29T20:19:38.742
+	thrust profile: [0.0037642309356178496 0.10817195619205817 -0.04203391806942476; 0.05018542722531452 0.011132758502156382 -0.0707574733140089; 0.01498586447762501 0.05712165647482545 -0.10331663549941099; -0.0021220081754707142 0.0427284404881686 -0.10738096661568876; 0.013851176936053975 0.06635540579133767 -0.11531028068050167; -0.03624664271973954 0.047411452014984014 -0.11058601864180033; -0.0020740631910354575 -4.710072118612996e-6 -0.1403320235583719; 0.004134084837005339 0.057833143727503075 -0.148726306245634; -0.000824882662939474 0.025545600899810554 -0.15811601473591735; 0.0033733625666936226 0.04310334955731879 -0.16265530338633763; 0.023284082987077983 0.07815514642145437 -0.14787129186662162; 0.011438920106420706 0.06298800208929839 -0.17089396585927522; -0.0028167264681480965 0.07221556852886035 -0.1682949193772566; 0.023003412445979414 0.07615232250394104 -0.12486622266414714; 0.05055936441931101 0.05061773551323538 -0.15558369926288854; 0.046376273514580145 0.05443645190395452 -0.15984218654287824; 0.02887318678938868 0.050242274973224 -0.11451690883278194; 0.05903220624034955 0.07663020899986919 -0.08872470614243323; 0.05646442157593271 0.0236833115162622 -0.12328998635670442; 0.052708769586655 0.04647341445165668 -0.08471778910840236] %
+Phase 2:
+	Planet: Venus
+	V∞_in: [5.03318023152429, 6.280182305174015, -6.060996943876664] km/s
+	V∞_out: [8.771878835411606, 1.7271436802598803, -4.64552460331829] km/s
+	time of flight: 1.2805978832351272e8 seconds
+	arrival date: 2027-10-21T00:29:26.742
+	thrust profile: [0.5166054641522004 0.38040574934818894 0.39483837842584535; 0.4828952263457908 -0.47829862312158744 0.40557553493743564; 0.6185006656113567 -0.4295308551988002 -0.3475134331936448; 0.4770039152011964 0.5271154524060135 -0.20000575030699538; 0.5412450144942943 -0.20886043145622096 0.43938036856081814; 0.5276789680667877 -0.5277616228639487 0.13628061369394617; 0.6415309466397165 -0.2678331791426979 -0.39558929497740725; 0.4343573860170071 0.502582921064376 -0.3318784701248486; 0.5800947529139152 -0.20204579937793274 0.3774150731579229; 0.5354834813587176 -0.4173102990305924 0.3796235568137587; 0.6184505220409655 -0.4417968378543587 -0.34238794209436774; 0.5080341201037585 0.5014345398019467 -0.33763169791467246; 0.5877098153802596 0.14114025736151312 0.3238083516450284; 0.5805187604081549 0.03982949798901487 0.38515870224511417; 0.5643130843803069 -0.5179163072176047 -0.19901273562840677; 0.618939895817285 0.389447844276657 -0.39925503596953016; 0.5411273409128876 0.3226806107049277 -0.37714997177083703; 0.6071744258656793 0.2911843912661802 0.28415164075125104; 0.5573265691088601 0.17823434208894331 0.4018394191685452; 0.5666337146024757 -0.5288498735192672 0.03819884543376086] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [0.7405450398567593, -7.5098445542472945, -2.40833325065344] km/s
+	V∞_out: [-3.959320578944167, 5.7458190962386, -3.749068046202953] km/s
+	time of flight: 1.421097770757432e8 seconds
+	arrival date: 2032-04-21T19:25:43.742
+	thrust profile: [0.6668749885535331 0.7119439515000974 -0.47217742545747104; -0.6469564667143733 0.7765188128496617 0.1574004795502485; -0.773633525867842 0.7394373999282712 0.4027317982639249; -0.8166053790607609 0.6473990001925622 0.5207562510569261; -0.8373014340476008 0.18359240688570228 0.5993895358042353; -0.8390303451637329 -0.42462892361099186 0.6142766346586279; -0.8350359388066501 -0.6239649730883396 0.6256719643517975; -0.821756634573213 -0.7144142912083659 0.6297147364166188; -0.7958608968982823 -0.7601769494789784 0.6210466135863127; -0.7510364885805915 -0.7850808235066821 0.5966784108754225; -0.6657999775087994 -0.7894095061990805 0.5609708009540707; -0.5101942765778178 -0.7782021262749327 0.5141768423449582; -0.27236357899533525 -0.7487127433927561 0.4618021651904532; -0.054244989960793334 -0.6945361755047911 0.4108890323914806; 0.025980362043212305 -0.6152046918846878 0.35533971599792835; 0.03884979852161373 -0.5000474202661694 0.3091329458166366; 0.0001114281549689611 -0.3447827035482281 0.256908008578505; -0.045624236967968704 -0.10554833156388801 0.20144441453096268; -0.09710696728868398 0.19152555422247225 0.1087766532370442; -0.1282579442088115 0.39646864777852725 0.009236041193641553] %
+Phase 4:
+	Planet: Saturn
+	V∞_in: [-4.741234768251964, 4.13190320501828, -0.5695428106723406] km/s
+	V∞_out: [-3.1515712454769806e-6, 5.189115178770385e-6, -1.6627213931492873e-7] km/s
+	time of flight: 1.8121908456931648e8 seconds
+	arrival date: 2038-01-18T06:03:47.742
+	thrust profile: [0.13625040297481736 0.14933905804631312 0.2757743121789037; 0.1192604239518539 0.14450577052892158 0.21001652823369818; 0.09497180738630677 0.1436206134610816 0.1304125477411028; 0.05660650818705413 0.14397646798764285 0.029638921674881153; 0.0033026815164827928 0.128393265450669 -0.08364054831257349; -0.046298739509475266 0.09498117676572271 -0.17204312101516736; -0.07826400300811034 0.05748675105859162 -0.23458089715837857; -0.0898822681455277 0.026068150966949772 -0.27381493027410114; -0.08817956687074757 0.003963795201985765 -0.29324311165103717; -0.08006421778460109 -0.010427589988313526 -0.297505213206217; -0.06850428258195482 -0.019821792080172117 -0.2909679340025451; -0.055774010972997286 -0.02726836207051607 -0.2762869825770171; -0.04157864032693081 -0.03339735152686053 -0.25548472609696515; -0.02660891319542901 -0.03894896063483435 -0.22960782433619792; -0.010643007042148598 -0.04490858196263294 -0.19956755059053796; 0.00580413466562435 -0.05025272650756578 -0.16582165226689483; 0.022646438724084665 -0.055672928642956324 -0.12919013606158447; 0.03956702474738428 -0.06069755736325737 -0.09167033305435902; 0.0569563523141951 -0.06556824149960896 -0.053646667488796825; 0.07561851012706877 -0.0723267563955561 -0.016753115096183893] %
+
+Mass Used: 2137.3878774591703 kg
+Launch C3: 35.71538607037856 km²/s²
+||V∞_in||: 6.31476921482568 km/s