Additional display functions and section 6 draft done

archive/non_saturn/EJU_2021-10-20T06:30:07.134/mission

@@ -0,0 +1,29 @@
+archive/EJU_2021-10-20T06:30:07.134/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: 1976-08-01T17:52:34.221
+Launch V∞: [7.796110966770354, 4.8982533648856466, 0.17379030255431946] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [3.8433311299973627, 5.796528049238326, -0.2817056847145128] km/s
+	V∞_out: [-1.50322449690382, -5.857435376892681, 3.4467617942706994] km/s
+	time of flight: 6.162384733838075e7 seconds
+	arrival date: 1978-07-15T23:36:41.221
+	thrust profile: [0.05076636324847266 0.044371172883747347 -0.000466591620230539; 0.04556839732559172 0.04551590000211736 0.026305580765275827; 0.04271388990028329 0.042965827861916495 0.032904618961254566; 0.04125704453812768 0.04399260927643073 0.011906508964846164; 0.037771810990335594 0.045126058811728244 0.017892630651311324; 0.03744914320857412 0.012083627702152488 0.016408253290893425; 0.037727702899229075 0.010853738248166893 0.015148025588847367; 0.005572973923857532 0.007303529249390285 0.011121028124084267; 0.00617297452148193 0.006145429794742058 0.011859116648542195; 0.005049233699504967 0.006452625990674288 0.011772625897474782; 0.004910258402799322 0.006366537658928831 0.0005643550152455212; 0.0025763592102966957 0.003181565085352132 0.010814482610218074; 0.0031947900522401847 0.0029830417754423276 0.011402488845003961; 0.0021986537890138565 0.0021185618970616647 0.011240126352455571; 0.0021605135862789084 0.0017022912732015678 0.011004028173214985; 0.0030322536190090267 0.0018820294472968568 0.011718419553167932; 0.0052532630469893085 0.004603904299207542 6.164903056357548e-5; 0.0024841647682658998 0.0010845905123058521 0.011858883503386769; 0.001563071377480838 0.0009462415703080935 0.011862566980378264; 0.005896854767673266 0.0028068208794427836 0.0011202252826535307; 0.002706071173844264 0.0007045991278482543 0.010364875508266558; 0.002614617358353478 0.0005047462925719528 0.011994006654582877; 0.003009332161874683 0.0005393209622101327 0.011846999130271842; 0.0029998210658897548 0.0006178369699748124 0.012638274768914527; 0.0018921149244373176 0.0006649354887339559 0.013988245401282478; 0.002177285891280997 0.0024857023352974046 0.006239009472882834; 0.0032550494781518127 0.0005709372281368296 0.014013879125368014; 0.0005852851857850025 0.0004382277614539412 0.015711382271976822; 0.0025298132080876744 0.0003394549467168767 0.015487289562849919; 0.002191799418810117 0.00044848314545440916 0.01576483894176832; 0.001933556956082662 0.00011480338097624216 0.017096420744044216; -0.0015516961136410024 0.00038972226556059235 0.018475608007619732; 0.0006938723421829548 0.0010956580579377906 0.010341674361039263; 0.0008683982111957906 0.0005679039999949838 0.018589985196626108; -0.00307180125243531 0.0008616727357253755 0.020309851014784653; 0.004028984608490049 0.0001817492649660781 0.012222080913189187; -0.004075416887687787 0.003505507802004826 0.020813135596843394; -0.004602868488561299 0.0017957581680285366 0.02205614447435787; -0.005119072302644164 0.003221591585835638 0.021534843370608594; -0.002774683023403968 0.0016034106418616914 0.008955547166790926] %
+Phase 2:
+	Planet: Uranus
+	V∞_in: [-2.38909099183748, -7.09851362908907, -1.4998494752601301] km/s
+	V∞_out: [-1.7579671813396809, -7.434026773843559, -0.5431781244031681] km/s
+	time of flight: 2.993961596792109e8 seconds
+	arrival date: 1988-01-10T05:12:40.221
+	thrust profile: [-0.07931776222154702 -0.09715466918867674 -0.026833250451506713; -0.09845323400323117 -0.17879388582940878 -0.04291406251121993; -0.08894254596894183 -0.09528460976651616 -0.054982106035208346; -0.06263720199951707 -0.0878116196248785 -0.05530652171544619; -0.06259005068834375 -0.09717952834183764 -0.06095027382199235; -0.06352579562023707 -0.09929139401807714 -0.07234338457248485; -0.0686236352886369 -0.09800849861144206 -0.08974924433995998; -0.05956649938146661 -0.08337006632048641 -0.1038431051473047; -0.04514195618670204 -0.08203823260227076 -0.10463027094106508; -0.06289461841109399 -0.060085191156628553 -0.10341360065396196; -0.05445769738916689 -0.09997930701298721 -0.09742267375781755; -0.05465737582266164 -0.08439167405860351 -0.09062236126374591; -0.04456643405680078 -0.07331795808665253 -0.09712534152461183; -0.06256760664966003 -0.08549758983692145 -0.12946096634923257; -0.06368110337977374 -0.0765333160455192 -0.12651913561849154; -0.06725919417261715 -0.09109284547953912 -0.12659879415802394; -0.07101397374081875 -0.08133483656944987 -0.046459438405158315; -0.04458830131822182 -0.06993359213652593 -0.10588197225202642; -0.043829644333553894 -0.06738613952355148 -0.10326501418112732; -0.043699162486397686 -0.07918563865614574 -0.09726736663887796; -0.041902410201523806 -0.05687746336476786 -0.09287616923343434; -0.05864620968926713 -0.045468494145468066 -0.08859391583215602; -0.03395345407232851 -0.03779592663169973 -0.08190251370577784; -0.032344510507555484 -0.03195310670080453 -0.07502124528522572; -0.02939009106005138 -0.027319895639058837 -0.07205569928293426; -0.02776511176948871 -0.02134845266988061 -0.07682410235978968; -0.025076508726846806 -0.01712782779219315 -0.06241551595889376; -0.023058918248386684 -0.011926231766031933 -0.056745466600086336; -0.02009516515935024 -0.007031029808761148 -0.051230718639702445; -0.011470301871887377 -0.004835200281315476 -0.04666627205144148; -0.008153291863800712 -0.009020456383335974 -0.04383434884087585; -0.0014098997805392169 -0.0026298096598901966 -0.03405966422871517; 0.014283781279323941 0.016279866267866545 -0.03609253084131848; 0.05336200053505927 0.03389800040998884 -0.040619525225581585; 0.06527766464651791 0.050216170197614575 -0.042586118795403936; 0.05723451861797406 0.03384400630020884 -0.03901891375575639; 0.08543313326117905 0.08974239510128046 -0.03621120917366133; 0.0630088316034018 0.15678763151906544 -0.005574987167467689; 0.060329780298105595 0.17485309892272635 0.013906868818896528; 0.0637300324111305 0.18467219733664741 0.016407349987587503] %
+
+Mass Used: 292.79309729930446 kg
+Launch C3: 84.80243530207245 km²/s²
+||V∞_in||: 7.638468430129195 km/s

archive/non_saturn/EJU_2021-10-20T06:56:05.706/mission

@@ -0,0 +1,29 @@
+archive/EJU_2021-10-20T06:56:05.706/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: 1976-07-29T22:56:52.810
+Launch V∞: [6.949925110063542, 5.51142706678786, 1.1338882248683144] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [3.906881971734985, 4.095747067849015, -0.40798750984197163] km/s
+	V∞_out: [-0.9527557058881729, -3.9759295150204843, -3.9356834360151556] km/s
+	time of flight: 7.564082964432266e7 seconds
+	arrival date: 1978-12-22T10:17:21.810
+	thrust profile: [0.03782916575140308 0.03740282492642642 -0.002576574442432617; 0.02568719536954076 0.06252477749229525 0.01652454606912066; 0.004225260108780641 0.03649507973713675 0.026304939794628213; 0.008514278978805623 0.005632465170283442 0.028766756627515436; 0.0028553869411493105 0.032931024849802475 0.02858849466203496; -0.00011527850331830502 0.037305718745844846 0.035357183754127365; -0.0020666322700494226 0.024839987547461636 0.04207353968844954; -0.0023476551667392757 0.02636000649838633 0.03519093267459137; -0.00833472270885205 0.020312456169983457 0.0354986543813712; -0.00428513003264013 0.019154229466167877 0.03662219548118329; -0.005892176333449648 0.018130402556353894 0.03636728290676028; -0.0042365610235936425 0.017010892842012324 0.03397204406749766; -0.004192371296486345 0.014784967560659735 0.023246181586815014; -0.004293857686960709 0.012931024770742552 0.03466591912622505; -0.0042609577287841555 0.014211942842773839 0.027172019947279497; -0.0036142056237695465 0.010452500777706587 0.04150772724566025; -0.003447004422321682 0.010358097537389374 0.02465859403683769; -0.0035755555454099917 0.00835659637766665 0.036388119539083476; -0.0013460117606815386 0.00782126057923672 0.03504230558583957; -0.003072300092481179 0.007188355933796116 0.03251483120438275; -0.0024662943066748387 -0.0358537525077433 0.02685483253738143; -0.001720854005330441 0.005884381838322623 0.03190085557916671; -0.0017412241063530884 0.007099738915174783 0.02682684424390216; -0.000920278204949286 0.005139980641523795 0.029434809365784742; -0.00033636789795050845 0.0036669219846624888 0.03287519625621116; 0.0007034209115346385 0.003501767722469495 0.028377718012140195; -0.0007434279012791565 0.002702853412641308 0.029244372161310265; 0.004866286278936821 0.0017203531584147828 0.02776349992801729; 0.0027504911079692476 0.001072925117832716 0.025680825527965283; 0.0020997450984179718 0.0009711597092673997 0.02061803880756732; 0.002173038215991327 -0.00014251845859543355 0.02156905284150965; 0.0015369099274299977 -0.0021290236096534283 0.021476611388992387; 0.007050352469994045 0.00016009300506752272 0.019346144543133968; 0.0041221682815360565 -0.0025995892998613556 -0.031065081280392186; 0.0053958554268588735 -0.002792436243787968 0.02051192181733026; 0.004118509542080822 -0.0035923393947791876 0.017414374655108224; 0.007861526059596693 -0.004103181354641067 0.014557072213757004; 0.008625807637409916 -0.005142988456101897 0.012197569085466388; -0.01306453843470772 -0.0038356113866674286 0.008329884768979636; 0.033014456775355874 -0.0045647936883905236 0.006863305832741281] %
+Phase 2:
+	Planet: Uranus
+	V∞_in: [-1.938316171288581, -5.830419960553641, 1.6937892024456043] km/s
+	V∞_out: [-4.518682402723378, 2.8551867184238096, 3.186319031020363] km/s
+	time of flight: 3.5891612134454197e8 seconds
+	arrival date: 1990-05-07T13:12:42.810
+	thrust profile: [-0.16989513619875685 -0.045677025710063386 -0.0030973835740971444; -0.1508597397272606 -0.05019563898711127 0.007204467510610183; -0.13420978791056495 -0.07142943296601216 0.018201689954637466; -0.11163546799447194 -0.08737032165349326 0.02732766258127402; 0.009113825963084335 -0.09585317692473423 0.05084952336647781; -0.09161229803325242 -0.09683650466428367 0.037082924841464006; 0.04125371110299494 -0.07680933686599022 0.0534261294839363; -0.07744796231792149 -0.04149385265133659 0.06712706717876639; -0.08943024907797331 -0.06791680699334988 0.07831568164802666; -0.07909240616228119 -0.06472558109648341 0.07290434329331255; -0.06743929900593662 -0.05897448140563983 0.0741408198271463; -0.07819359845202928 -0.06647016191133999 0.0660436817760916; -0.09613068470236329 -0.059166161100852675 0.08060714904979402; -0.07312572091628138 -0.05693061246215791 0.07436389578550606; -0.027570631599454522 -0.059342090803171155 0.07347329358087554; -0.08317002523720268 -0.061818515844878186 0.041467954236152335; -0.07583390698096582 -0.06567919479648035 0.06873073575145; -0.08204408482821308 -0.06168526249705727 0.017377533255748923; -0.08177518700808466 -0.06338581414826097 0.08609161332719108; -0.06598866513441994 -0.07232579202499327 0.06692776564855539; -0.06347014466905312 -0.06414871849237591 0.07897242421747777; -0.05978263664535798 -0.06933208486458832 0.07722271340402495; -0.042839660913592426 -0.0691467820960932 0.0792489224821808; -0.048220787215069935 -0.06975611644646947 0.08493324999489961; -0.049101088565368545 -0.06513558156977915 0.06154355863275868; -0.05585227084219764 -0.058795508980296285 0.07222729242954258; -0.059679510740878634 -0.05037068555696405 0.08573889901755061; 0.05943101681925227 -0.03346975509652526 0.08296424618848902; -0.002011173439567788 -0.05294783680627407 0.0794657562790766; -0.03132595187332769 -0.04585581870208009 0.06847870733055934; -0.029172177173713672 -0.04911166397541467 0.06900916577586096; -0.03419181581676224 -0.050997881676723304 0.054162115369051175; -0.03952854899176259 -0.036375329108467025 0.04088691066500227; 0.07317701734795691 -0.03019477676470679 0.017070982033922204; -0.03660809431367548 -0.03709092568306137 0.042140497725608; -0.03373273474707058 -0.04779512940475388 0.026504620225648024; -0.04557909599180323 -0.02516006761801134 0.020229804898252192; -0.039048523770669794 -0.02375522303243242 0.01420415637304866; 0.013208543377162343 -0.0032720049019988547 -0.007729033179125844; -0.057959608471409775 0.0007246097139177125 -0.011729486022561447] %
+
+Mass Used: 324.65554095417156 kg
+Launch C3: 79.96298985450858 km²/s²
+||V∞_in||: 6.3733655440922625 km/s

archive/non_saturn/EJU_2021-10-20T09:24:50.637/mission

@@ -0,0 +1,29 @@
+archive/EJU_2021-10-20T09:24:50.637/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: 1976-08-03T18:07:52.908
+Launch V∞: [6.299916182319705, 6.240538451377015, -0.9940165103728982] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [4.178807865103526, 3.271316108925791, 0.038831033060078735] km/s
+	V∞_out: [-1.3778027301160083, -5.1110224704243725, -0.38018528529187656] km/s
+	time of flight: 9.076893335112691e7 seconds
+	arrival date: 1979-06-20T07:43:25.908
+	thrust profile: [0.04513213164333234 0.04346394223048948 0.007180644066023622; 0.023711461445665785 0.04851693214299602 0.03207463889343553; 0.00969082323802968 0.0429167126574647 0.05027917371754633; 0.0006490219093697312 0.03432108495203708 0.05302050429400685; -0.003953708767625976 0.02834092045678569 0.05567795776724263; -0.007078446275295329 0.011750260516732298 0.05750557980134808; -0.003435272692576073 0.02122406642664124 0.06262312885175245; -0.009695677074664703 0.018479022813936753 0.06053735694521427; -0.01142145238531702 0.015117586694892556 0.0638000808444341; -0.012068039284864305 0.012122660566706385 0.06391205556608177; -0.012302230314909514 0.010908149372005694 0.06019740157959107; -0.01446161436665235 0.008373928351474595 0.059323058345291314; -0.016583035763738076 0.006299387290095585 0.06082959992214257; -0.01706759812967117 0.0065044105221593 0.05778343872547179; -0.019486845820007016 0.002193974387266614 0.057393172584176734; -0.020473650886052644 1.380648034282904e-5 0.05731896545245807; -0.018767281384997753 -0.001918872534461376 0.05612361619283167; -0.021591450801765708 -0.0042488196125658765 0.05450598919383925; -0.021478255013919884 -0.006464299578735615 0.04809767450620565; -0.022653919145895585 -0.009019740247343862 0.048362756123037046; -0.023544833613709452 -0.011660942116303467 0.04427505897015856; -0.02487650131449469 -0.01482208132042167 0.042971426063402186; -0.025304632579721677 -0.017024463752791045 0.038971334825125444; -0.02627710448532682 -0.01999518763372068 0.036273080926672384; -0.026409220881850253 -0.022340756335864343 0.03346167188312444; -0.027035811169801346 -0.026330622264995978 0.029551995901678153; -0.027294988215502632 -0.028965874411855858 0.026920943329044964; -0.02543100070917406 -0.031206127791626466 0.02244980247094962; -0.027031341088425847 -0.0340466798524574 0.018998557859187092; -0.02741737072358986 -0.03790113735478487 0.01557337910538438; -0.0272602309532185 -0.0408499812859817 0.01194792933774343; -0.025909850501463313 -0.04396390625007793 0.00813014729889798; -0.02506976623031212 -0.047397447305083704 0.004665530910703655; -0.023334361066159846 -0.048678373843736196 0.0009546486525111172; -0.023889478406793792 -0.05679728290807836 -0.002589587233405526; -0.02724340418820601 -0.05816253276542619 -0.006122379800579124; -0.021218565581682256 -0.06185180447607849 -0.009044740289425488; -0.019380826507997755 -0.06887292315771941 -0.013887128275611392; -0.01630947060752653 -0.06863416874846709 -0.01479387901178276; -0.015411951104633738 -0.07135904293057543 -0.01714932934975381] %
+Phase 2:
+	Planet: Uranus
+	V∞_in: [-1.845021665733062, -5.678663565100718, 0.3029957863298556] km/s
+	V∞_out: [-3.909849414959923, 3.5759430497442013, 2.370770023155677] km/s
+	time of flight: 3.08114874485728e8 seconds
+	arrival date: 1989-03-25T11:11:19.908
+	thrust profile: [-0.06674811641031352 -0.05612757204576699 -0.027545219420525784; -0.05559395467233815 -0.05898058463022347 -0.027618778760360937; -0.05692889817706908 -0.06138740735669628 -0.024127884156966553; -0.04938597114969373 -0.05897632826574441 -0.020875930634551777; -0.04513949441889156 -0.05493677886831321 -0.017744255550718353; -0.04191267048560369 -0.0497040919280347 -0.014850616507294535; -0.03951131641179269 -0.04341382786449151 -0.009778820274569259; -0.0370863829866412 -0.03639713660534706 -0.007535292090010591; -0.037410692933588605 -0.03106890983815507 -0.0035126740989491565; -0.035384789101130805 -0.02554445172882075 -0.0017983914198710438; -0.03574977327075396 -0.02113010504624859 -0.0001328491376689744; -0.03194724079988652 -0.01638421067813942 -0.0011505498097668584; -0.034180716278068 -0.013877672988327941 0.001627089350782669; -0.03885278128497657 -0.01161056124179592 0.005447519394925048; -0.04780658577496266 -0.009642777483071765 0.008770370725385047; -0.039523274181837605 -0.00583266582504645 0.010285929551974837; -0.04054425271649562 -0.0030979021814110763 0.013538087528531879; -0.042081635316423546 0.0002896039819797671 0.020386417210395406; -0.04163111462438231 0.003378109131498211 0.018796072247663165; -0.04381682122520203 0.007198467572032381 0.024926690546142397; -0.04521110915147108 0.011920408867649519 0.029020217823105928; -0.047873959213738576 0.01694996877307094 0.029539969915417366; -0.04789681559790685 0.023080413175950897 0.03548445565572181; -0.048968821642495 0.031283457963523637 0.042288153133598176; -0.05513570922771978 0.04188862330873962 0.04315061325522542; -0.0460427824369968 0.05532672923356575 0.052911791351016764; -0.04595007962041501 0.0682098780156651 0.0545332693961846; -0.04020043790691544 0.08884049852098926 0.054905659724033544; -0.03406076232020952 0.11144075206336615 0.05094487923514953; -0.024252121467827105 0.12900503386624168 0.05115224879295048; -0.0176104293681911 0.06260126480105925 0.04470427127414733; -0.008891011397626766 0.1312405594766333 0.03624981025811338; 0.0004454420607871681 0.07329672426875136 0.03146945127603886; 0.0024886701231228332 0.1417457581542488 0.02033654814598019; 0.025071362315817032 0.19698210332984226 0.021196655967815694; 0.0324021609887447 0.15074081889051183 0.0034214591933819246; 0.03632243807074882 0.15207933955719707 -0.002120489459561229; 0.039403691731321876 0.155368573708892 -0.007770585754213655; 0.044300010743546385 0.1656092696295884 -0.009813911794334952; 0.04940888045966933 0.15430255903950427 -0.013461557013245747] %
+
+Mass Used: 254.85590261239986 kg
+Launch C3: 79.62133289026262 km²/s²
+||V∞_in||: 5.978555952666198 km/s

archive/non_saturn/EJ_2021-11-07T14:46:30.627/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EJ_2021-11-07T14:46:30.627/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2022-08-22T08:59:30.624
+Launch V∞: [3.8443592907721276, 2.9537837181042104, -0.013562913535938395] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [3.544527650191706, 8.397825652752136, -0.35643002951529873] km/s
+	V∞_out: [-0.6639013930157557, -0.21397258559898233, 0.0012758806822037029] km/s
+	time of flight: 9.72503999711726e7 seconds
+	arrival date: 2025-09-20T22:59:29.624
+	thrust profile: [0.309005048551296 0.18339415892490127 0.0027002374517968134; 0.39038340279454015 -0.08598467958258589 0.010312803693732317; 0.44938940212387873 -0.08807777402752429 0.002785661604362881; 0.4727841039456793 -0.03534032379035236 -0.0018849144811814039; 0.4690712072738283 -0.03960532320766157 -0.004473107597690517; 0.45397991987657443 -0.15486398878325663 -0.005680521852703244; 0.4485788241679923 -0.33567734538476923 -0.005564951845911451; 0.5216248999417937 -0.47975370744057766 -0.005660397120411834; 0.6920392190397051 -0.5005798311516338 -0.005517054932513914; 0.7679838906703794 0.5300520361001183 -0.005384387857015156; 0.512203310002801 0.7194823119304291 -0.0013647498450424262; 0.10514790861349814 0.6588219176238146 -9.159548578737903e-5; -0.049683494944089746 0.566183781136383 -0.0022586868669512107; -0.09075248681288331 0.45610022500744607 -0.0048523160949628065; -0.09113418145248406 0.32137343790235245 -0.0070576027907159975; -0.06362403013939313 0.1616622098305713 -0.007141491746951609; -0.026630089589957294 0.06904180653539292 0.045229599639996836; -0.03213597234268758 -0.03832310884384863 -0.04027384190804232; -0.04777262750501482 -0.0880912585120324 -0.008201840560253705; -0.06646385015927217 -0.2585191874042375 -0.01264613200500041] %
+
+Mass Used: 1647.839085407878 kg
+Launch C3: 23.504120562507094 km²/s²
+||V∞_in||: 9.122181445407433 km/s

archive/non_saturn/EJ_2021-11-07T16:22:00.626/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EJ_2021-11-07T16:22:00.626/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2027-11-04T12:48:56.123
+Launch V∞: [-8.732498886729314, 4.51787497134938, 0.8120510695970266] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [-9.88645331410529, -0.7687768634212618, 0.7151206660880595] km/s
+	V∞_out: [-0.4049088507623607, 0.17689076088451985, 0.12508940089378756] km/s
+	time of flight: 4.573440000016084e7 seconds
+	arrival date: 2029-04-16T20:48:56.123
+	thrust profile: [-0.7252261699958953 0.6373188434471561 0.4327846850623052; -0.7899362435001571 0.3285194444697549 0.11446253449938033; -0.7680712363242684 -0.1633173479005095 -0.0753102013115445; -0.5201123290608496 -0.42217681987872474 -0.4647696966643137; -0.6013508181063658 -0.38366831483797026 -0.18445814629025725; -0.4581606987896879 -0.4855808976013353 -0.15444850808484772; -0.37205177911023174 -0.501948737017628 0.21622379964927294; -0.1781544080297839 -0.4306466711988113 0.3202277932838901; 0.12501657753821185 -0.27972314722739877 0.28303296476247813; 0.4191923487620815 -0.29573006731278095 0.20455931421399057; 0.5792812793607826 -0.268749218378091 0.15158178555333274; 0.6702069008818273 -0.24258440317814584 0.10970704007148652; 0.7255027823505624 -0.20038844589657145 0.08179428268131272; 0.7651208085523874 -0.1256488783092542 0.0635390724723628; 0.7950141678580656 -0.03125730833494034 0.057007373036390994; 0.8201460826806802 0.04826201181747142 0.0601673546745067; 0.839804313083261 0.08886942147745636 0.05911914379889547; 0.8565227352600031 0.11422389861125826 0.05311635951607426; 0.8680126164067367 0.13837977169566942 0.04826407864677627; 0.879590709240378 0.17035725114157071 0.043746933343917625] %
+
+Mass Used: 1262.655513556444 kg
+Launch C3: 97.32715800310754 km²/s²
+||V∞_in||: 9.942050822882647 km/s

archive/non_saturn/EJ_2021-11-07T16:23:30.327/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EJ_2021-11-07T16:23:30.327/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2027-09-12T06:04:50.667
+Launch V∞: [-0.1356894386368732, 5.956064811848478, 0.01939640608336112] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [-0.2571115997565001, -0.23716727061524712, 0.1301306668580519] km/s
+	V∞_out: [-0.014179189011866182, -0.008514489265672389, -0.020254493877991896] km/s
+	time of flight: 1.8070773341225305e8 seconds
+	arrival date: 2033-06-03T18:40:23.667
+	thrust profile: [-0.28796335426441344 0.2918284262842529 0.004232031537641381; -0.4146826747229724 -0.02204183876659545 0.006463923516828132; -0.3658131284334198 -0.20897490324756807 0.004830213098433344; -0.3009950427607718 -0.29983050286376706 0.0026330364724320627; -0.21226927941652138 -0.31438885498847047 0.00016223993548310865; -0.13803056237326825 -0.31060963133872505 -0.002084476169128304; -0.07968485985716361 -0.29051876651351477 -0.004227991069940268; -0.03393237770799525 -0.2616050729753513 -0.005805065906776818; 0.00010399437044312852 -0.22612386906622065 -0.00723203544008763; 0.02431397619795949 -0.1841020095991609 -0.007967346627807494; 0.03387857848006785 -0.1473548203513266 -0.008904505604898574; 0.0464200796450669 -0.10786650792140276 -0.008591232690818134; 0.05146001248652659 -0.0649385531036076 -0.007930560486331771; 0.05288431148130223 -0.014078912962736419 -0.00441593039414774; 0.0455197215338432 -0.024008992010477768 -0.009803033072905896; 0.05520804599773281 0.0034148633177632287 -0.0036277778862629463; 0.045785853836455455 0.00794833182192021 -0.0217178944298006; 0.04513924118080819 0.05766612276661263 -0.0007249356261771857; 0.0848074300734865 0.06484381201504433 0.010866963214099381; 0.08645863137101507 0.10712102831006817 -0.005895302546374282] %
+
+Mass Used: 1398.921932467841 kg
+Launch C3: 35.493495887266185 km²/s²
+||V∞_in||: 0.37321398612237705 km/s

archive/non_saturn/EJ_2021-11-10T17:36:57.486/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EJ_2021-11-10T17:36:57.486/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: 1977-09-23T03:22:48.372
+Launch V∞: [-9.493171911757265, 1.996521857385693, 1.8459560902623946] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [-9.543974938238337, -5.087831983949424, -0.35708404363703494] km/s
+	V∞_out: [-0.129298458647144, 0.15324446409210052, -0.009200490470804264] km/s
+	time of flight: 1.776357220782331e8 seconds
+	arrival date: 1983-05-11T02:38:10.372
+	thrust profile: [-0.7610489826673982 0.4519575670810889 0.38105436601704845; -0.692182777203481 -0.5430220362690558 -0.19169924364371457; -0.713848909301823 0.5682383712035098 0.21475368591818692; -0.762202012287276 0.6169631842658447 -0.06393276641993992; -0.7682887422768392 0.5658174117175422 -0.356299726756724; -0.7247484323513448 0.615681193372203 -0.3204930084782787; -0.8443101955436311 0.7531829445331782 0.35162106487694683; -0.7361591502293401 -0.7428403909252584 0.054461158094787014; -0.6989134861291908 -0.542824582709043 -0.07047657066876702; -0.7311534977516068 0.308382219231665 -0.2420265209340023; -0.7433256599203858 0.5382732546276702 -0.2395625345263195; -0.7439731882157303 0.6152077332897807 -0.2615422771160056; -0.7183921784988241 0.683166135255115 -0.25632068075573156; -0.6372607269354764 0.7800738376092019 -0.09467864945511045; -0.9264981728556586 0.8626484815884095 0.7406409970321504; -0.6596702419789453 -0.8411615509502441 0.18958949263763294; -0.20841320586198334 -0.7908230728915269 0.12046929919930525; 0.26398550226277 -0.7164725093202939 0.085019685455708; 0.4864448421040628 -0.5765963344719907 0.052561242827218184; 0.6036699781228905 -0.23314430271586686 0.02081945694704924] %
+
+Mass Used: 1364.498204540083 kg
+Launch C3: 97.51396636037275 km²/s²
+||V∞_in||: 10.82132158901307 km/s

archive/non_saturn/EJ_2022-02-20T15:35:42.756/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EJ_2022-02-20T15:35:42.756/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2027-05-07T16:42:16.204
+Launch V∞: [1.7378678187417211, -2.46862158520496, -0.6330916686471314] km/s
+Phase 1:
+	Planet: Jupiter
+	V∞_in: [-7.0779894637956104, -6.322884251065928, 0.08249231159415504] km/s
+	V∞_out: [-9.886721268095892e-5, -5.2044547868849095e-5, -1.4279616788653462e-7] km/s
+	time of flight: 9.753480002947423e7 seconds
+	arrival date: 2030-06-09T13:42:16.204
+	thrust profile: [0.3496133127402798 0.21627658848562392 -0.09375257020030825; 0.33049519901462543 0.4914216730807561 -0.04333085534469271; 0.015695434994927256 0.6376829912952088 -0.010776108385759698; -0.44272307995336146 0.6725191353780019 0.02401109287371488; -0.6273162232623738 0.6534499707573249 0.04855355942035699; -0.7062446552268619 0.5648886015889624 0.06359834741284556; -0.7337027908428936 0.34137315135163543 0.06893276201071429; -0.7263479369913934 -0.04280550187252788 0.06504582329795826; -0.6907323077547943 -0.29916252254363473 0.05655854617201239; -0.6304099965747246 -0.39539357580226175 0.04777470251604466; -0.546644598339376 -0.41045795909146016 0.03986867238422301; -0.4449769658797206 -0.3791551577739326 0.03302815362892815; -0.3343801111760648 -0.3170155537328812 0.027015156520834947; -0.22238014374440118 -0.2330409572673364 0.021363765089885373; -0.113202981166323 -0.1334888611558203 0.015342498857529623; -0.017481222034237697 -0.026432427062662682 0.0036199536612145674; 0.00010928351095286555 -0.0017246713395881355 -0.002344486658782495; 0.0003606569072872833 0.0017587019964605832 -0.00047445201553678664; 0.0018193454249226754 0.0015129170111366306 0.0008999344832791579; 0.08640210944237164 0.058949618519573616 0.004429993495706424] %
+
+Mass Used: 1720.4129974933717 kg
+Launch C3: 9.515082147268366 km²/s²
+||V∞_in||: 9.491238332454378 km/s

archive/non_saturn/EMJN_2021-11-29T17:22:43.432/mission

@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJN_2021-11-29T17:22:43.432/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: 2024-12-23T15:19:18.306
+Launch V∞: [3.7246340359905252, -0.7668922286241167, -1.2982795287623152] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [2.494283608647667, 0.4779176399654301, -2.4127945752092663] km/s
+	V∞_out: [-0.4965998694292626, 2.280726103742723, -2.6122161933665495] km/s
+	time of flight: 1.1112593378745796e8 seconds
+	arrival date: 2028-07-01T19:38:11.306
+	thrust profile: [0.574314864465574 0.4270452174232693 0.29638159374668793; 0.5446571483586893 0.6545005999072503 0.29885454938460493; -0.6407008818388138 0.6047471705598826 -0.3611107482397214; -0.6090910018886806 0.4086292020353647 -0.3182239029023878; -0.5972700374128047 -0.5925649766181501 -0.1428611882223418; 0.7035933873557789 -0.7374496458897967 0.25856313264181247; 0.6187581048385012 0.71068635783626 -0.05789366680034934; -0.6641950503565809 0.6437898522192934 -0.27526162728737996; -0.7420417902057971 -0.41426865914506017 -0.23642243903474278; -0.6117186284649462 -0.7691378662390483 -0.008551868685930122; 0.9103799821363571 -0.6958464571429571 0.20143430274286617; 0.6949604843307996 0.7921653784196445 -0.06766318190720352; -0.711280843553026 0.7699727320198064 -0.2712015558254371; -0.8157341118174929 0.47411989191797727 -0.25649460581099315; -0.8017585640901678 -0.7742154973052455 -0.037675698291696834; 0.04044429011740304 -0.8663007134481628 0.2032563083072973; 0.854373492928133 -0.7735870663242215 0.19757822091240435; 0.8364988214950911 0.8495507135624523 -0.07245450181745107; -0.17309103497250355 0.8763214931380413 -0.2655879782455708; -0.8411527513899564 0.819160378514693 -0.2586467736093903] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-5.538205957708029, -2.9054361894143304, 0.33552637947187924] km/s
+	V∞_out: [0.5046777525076017, 6.240066179835522, -0.1810924190839511] km/s
+	time of flight: 1.5845886601650202e8 seconds
+	arrival date: 2033-07-09T19:59:17.306
+	thrust profile: [-0.9036543510864951 0.6541143791625612 -0.3222980415291042; -0.8832461130197783 -0.737424683011361 -0.3022522605581414; -0.8209657934438149 -0.855511836631351 -0.2551798333859342; -0.6867673786369394 -0.8683395906979817 -0.2263222463630974; -0.4869220845452508 -0.8445214158833173 -0.20970174656218277; -0.20841896070390353 -0.7994903923698052 -0.20870160122576703; -0.013585575385545936 -0.7383743288456648 -0.1919873808978343; 0.04620627341952782 -0.6700807074028765 -0.1848557385194478; 0.049421838780437675 -0.590097708762824 -0.1747481413522336; 0.012575602179280861 -0.895741483645297 -0.1611163452378958; -0.01613975443303747 -0.4787302006004795 -0.15227094975068786; -0.06374834913614788 -0.41745586732624557 -0.13522213977947276; -0.11463100448525404 -0.36122938863930504 -0.11744005758165722; -0.1621639112103503 -0.31724876310417627 -0.0958874392701142; -0.19648220854838322 -0.264314663849154 -0.066076328071633; -0.24485223518636903 -0.1836441254903296 -0.04896203316737631; -0.2546968905066618 -0.16905466281492817 -0.022816834037144577; -0.26867493243738294 -0.11533995019061173 0.003308757184394887; -0.32378451108160405 -0.03869230342562393 0.030203817435557827; -0.32950610082115867 0.026204868836291285 0.059545893198771155] %
+Phase 3:
+	Planet: Neptune
+	V∞_in: [9.265725092936133, -9.786832491497965, -0.08265318279988049] km/s
+	V∞_out: [-0.04939156370003244, 7.080398077984083, 0.008343683362610646] km/s
+	time of flight: 1.1790191001194214e7 seconds
+	arrival date: 2033-11-23T07:02:28.306
+	thrust profile: [-0.03898824639829615 0.16371784077873527 -0.00013552715761737044; -0.03965980066394493 0.16534224208941117 -0.00011383530680316276; -0.0408187339699479 0.16443725546158428 -9.400453754275044e-5; -0.041109678864468216 0.1647205038566749 -8.342084332467601e-5; -0.04174133700362553 0.16664340240392897 -7.006086027666118e-5; -0.0424810737661852 0.1667002978899254 -5.700029092451851e-5; -0.04239207210941273 0.16701251418502575 -4.383623068936747e-5; -0.04652037459029391 0.16804035967999092 -2.978584844002596e-5; -0.04427137548076659 0.16950248273838245 -1.5426422905404063e-5; -0.04508723711412531 0.16561986502047163 -1.3433623473967066e-6; -0.04558502556546034 0.17116968335570643 4.062370321680114e-5; -0.046116752045498706 0.1722075533700207 2.3987312014333166e-5; -0.04709823531387585 0.1715653407790682 3.545164619148473e-5; -0.047773360118737326 0.17247757474396616 5.171911800828078e-5; -0.04877410118731465 0.17444398529369937 6.339628403937785e-5; -0.049033599874160665 0.1739487314179798 7.666428673687004e-5; -0.050091444345239274 0.17443171851273329 8.994289395414832e-5; -0.05049095135560994 0.17620949694675078 0.00010428768262633634; -0.051247933732248764 0.1760232752199048 0.00011912360582272222; -0.052158341276396 0.17808218005608098 0.0001313980216301485] %
+
+Mass Used: 1726.4616690486366 kg
+Launch C3: 16.146552127186432 km²/s²
+||V∞_in||: 13.477484307656734 km/s

archive/non_saturn/EMJN_2021-11-29T20:07:38.430/mission

@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMJN_2021-11-29T20:07:38.430/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: 2023-05-27T23:45:19.477
+Launch V∞: [0.07060914008148668, -4.847892797001834, 0.5290687721885886] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-2.8376948696397957, -6.866970594886355, -1.1016914014907047] km/s
+	V∞_out: [-4.226081909733871, -6.202110186999845, -0.3094281797413773] km/s
+	time of flight: 1.596037143160738e8 seconds
+	arrival date: 2028-06-17T06:07:13.477
+	thrust profile: [-0.08820762853917691 -0.14898517184082533 -0.09820752341370556; -0.16244500639383114 -0.007014189727643575 -0.042114530446779465; -0.11504442623490056 0.058307478489750215 0.012249450040533938; -0.17383665852971933 -0.02660802135748719 0.026296611919654635; -0.133605782067695 -0.18132533878993642 0.026002941407235212; -0.04006331095609107 -0.20273912830830298 0.004427347789879819; 0.10608908750365087 -0.14243574598913397 -0.040859364773162925; -0.1334058871429112 0.07395229686780111 0.017691464102652134; -0.19635497913555464 0.04582057433286239 0.014753056279381485; -0.22659830579310275 -0.1361676942645219 0.028039092180629516; -0.056452159199491696 -0.282304137567597 0.01760271375341965; -0.055869205300458795 -0.07521165313474892 0.07001754063761095; -0.10815326401024924 0.03975665673607279 0.08633566772197054; -0.15411574858207477 0.11420315814948176 0.020068825808757306; -0.2842273817584412 -0.0034013997105323997 0.024345468294325344; -0.1943513861122515 -0.28856449475866197 0.024667879112035683; 0.06001359666756579 -0.2750814648121676 -0.016222720706101045; 0.1634047690981133 0.0633323684514685 0.037052952793005536; -0.06358457091065511 0.19606506430779863 -0.061016941617662156; -0.21816429202004126 0.10669767546640854 0.03444638959744015] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [3.7354750271686217, -5.88285076118926, 0.3565930630644914] km/s
+	V∞_out: [-0.34319042907183317, 6.967067331497001, -0.17523613192719362] km/s
+	time of flight: 1.599110498440805e8 seconds
+	arrival date: 2033-07-12T01:51:22.477
+	thrust profile: [-0.40987114064695546 -0.3774240932862401 -0.03561424162645277; -0.3658595283634409 -0.649925100592242 -0.03267051158991308; 0.3459098563469254 -0.6438693437660852 -0.04635788737542222; 0.5043654957163684 -0.3232526513194753 -0.01450355602555917; 0.42491000056144884 -0.21802276807884619 0.030992274127171215; 0.34082656017644314 -0.17376917376621892 0.04325816043964533; 0.1376056849711479 -0.12166741048661384 0.05225660923751248; -0.13620705214465267 0.022867431783402784 0.06787427526509686; -0.3502016747280746 0.1254089210892246 -0.03219035055838345; -0.7729039185116515 0.050166197257457634 -0.07418896319497846; -0.8826906384645422 -0.42770154496434787 -0.09066661080452741; -0.8697879488343527 -0.8989912582247904 -0.11292428779799557; -0.3012587410720149 -0.8933703434566561 -0.10271304251295864; 0.7595659924014233 -0.8695220977621636 -0.049116949463447176; 0.7872267924160511 -0.6662320332198877 -0.011350265126440771; 0.7392293426195585 -0.33787052962012654 0.00950541251523341; 0.6603814845566363 -0.005691408214699979 0.01737841943566633; 0.5573136293405954 -0.158764215359649 0.021196329449577604; 0.40957430642093684 0.1915873694381741 0.028239988792705437; 0.18146188186458964 0.1883476561832824 0.03330416774233607] %
+Phase 3:
+	Planet: Neptune
+	V∞_in: [8.506155596263332, -7.214120420207235, -0.09860913292565265] km/s
+	V∞_out: [4.053253594386909, 0.1372094566434354, -0.11675704795783998] km/s
+	time of flight: 4.156831849103214e7 seconds
+	arrival date: 2034-11-05T04:36:40.477
+	thrust profile: [-0.04831977082461104 0.02886785140102746 -0.0015969011424151007; -0.04917765507361394 0.029203456393022745 -0.0014934586981430707; -0.05007927680116305 0.02937008233469106 -0.0014606345664627358; -0.05064789643929198 0.029683169999243322 -0.0013262520866866735; -0.051317004632228186 0.02971960728170897 -0.0012160227437881396; -0.051520874234056616 0.02977614467368215 -0.001115494384017753; -0.056261871812928875 0.03168558834789489 -0.0011825214765981728; -0.05393084917042745 0.030529761089447334 -0.0010052780980467106; -0.0545540520950892 0.030843664255386857 -0.0008871465845663635; -0.05481610839179922 0.030675652290316765 -0.0007096252268282277; -0.05535607825958336 0.030792442226543953 -0.000613617898828771; -0.05621636785416013 0.031177946238027898 -0.00048131038774713544; -0.05674803704179758 0.031109150076321142 -0.00042081760152222307; -0.057490162528803464 0.03146649637736389 -0.00031633576187554854; -0.057978129725565604 0.031470064297792776 -0.00021040663675848088; -0.059695605398968794 0.03214040241964867 4.28282466982456e-5; -0.0598515487471952 0.03219101178897971 -8.932622689143771e-6; -0.060385880377208864 0.03228344074846185 8.425209789811808e-5; -0.06140170323745024 0.03255841183319602 0.0001927115343330996; -0.06185254886048141 0.03268815199448967 0.00029588992432612673] %
+
+Mass Used: 1125.3822536870607 kg
+Launch C3: 23.786963987590454 km²/s²
+||V∞_in||: 11.153830742224367 km/s

archive/non_saturn/EMJSU_2021-11-11T04:50:20.773/mission

@@ -0,0 +1,43 @@
+/home/connor/projects/thesis/archive/EMJSU_2021-11-11T04:50:20.773/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: 1977-08-29T00:28:42.235
+Launch V∞: [-5.993015939919875, 2.5730948883971196, 1.0995056788128965] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-4.912918793015281, -5.749282630615395, 3.500451711966386] km/s
+	V∞_out: [-3.4658376295259443, -6.128480904546313, 4.458055817928218] km/s
+	time of flight: 9.655561330465347e7 seconds
+	arrival date: 1980-09-19T13:28:55.235
+	thrust profile: [-0.6848479340229933 -0.6317473532438761 -0.6789410387377113; -0.7283373129568128 -0.6597015909585692 -0.6860291664652663; 0.5143122109172585 -0.7554166841816019 0.6548911297971178; 0.650987105546092 -0.739938250992294 0.686244011796856; -0.567349081163571 -0.7171322204555259 0.7176501535009572; -0.6060664652754209 -0.6881472823274762 0.7152061841403491; -0.6457752364426499 -0.6793453331017747 0.6901800477645527; 0.6373998427205125 -0.6901370973195071 0.6440943571979044; 0.6232981297616063 0.6245585478937647 -0.7042650672249426; -0.7173110561506139 0.47022815205529234 -0.6937264189108627; -0.6298819082617076 -0.7335307650242696 0.6794508601033687; -0.5840798229168693 -0.7117652775560642 0.71673753565496; 0.6518652084909865 -0.679625481136191 0.7150981814535525; 0.6269343446266082 -0.6783434977916609 0.7005711370434008; 0.6192953242902497 -0.6895768905181153 0.66192822798728; 0.6249355751156056 0.6111710277362319 -0.6978924565831346; -0.7127959821946511 0.5739058413985498 -0.7071394367657958; -0.7027946745383137 -0.7495505439357887 0.5974000176561298; -0.5796183131865142 -0.7574601098030497 0.6961759879457895; 0.6831171982226909 -0.7168789234373818 0.7163908572195994] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-4.687613669172795, -9.137643103467221, 2.7610043724460294] km/s
+	V∞_out: [-6.84902175973724, -8.134664345135159, -0.10743273528963516] km/s
+	time of flight: 1.0295640390127918e8 seconds
+	arrival date: 1983-12-25T04:28:58.235
+	thrust profile: [0.6995410218848744 -0.6393230267422165 0.7647526533373915; 0.6698438420960121 0.7948373479414468 0.7488466112399416; 0.6133803630656508 0.8721432241652148 -0.10503387899547705; -0.7975752189273541 0.8967673181002215 -0.620565856208428; -0.8810777959243058 0.9109617670598268 -0.7447072404898911; -0.9255982733383775 0.9048235938487734 -0.81044200796326; -0.9451974194019941 0.8324645836800456 -0.8403473305611608; -0.9491498129909374 -0.8041118034787202 -0.8374748559038501; -0.9403374896987303 -0.9097804605905754 -0.7972210189785967; -0.9169616625063207 -0.9275441774549357 -0.7103882336630395; -0.8728172615404418 -0.9276214940959352 -0.5569943225350228; -0.7993897280663421 -0.920066591499417 -0.33089228095477646; -0.6888132887887403 -0.907363288341434 -0.10712622625205351; -0.5426334991349746 -0.8897807303349454 0.01545869967612042; -0.3845125217852459 -0.8660959201232201 0.0595623181632033; -0.25074420932651464 -0.8328879482223247 0.06618674123489034; -0.1562010398806513 -0.782506799826215 0.05663281267460723; -0.08963029099274077 -0.6955803608136205 0.040725635567769376; -0.03579683914976781 -0.5103095698513694 0.022483515806162563; 0.054945234199508655 0.14977661902108105 -0.025469760738754343] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-6.161620202786709, -3.655571526334963, 0.5856830695389122] km/s
+	V∞_out: [-2.7002022006751494, -6.66028396264326, 0.14619073909240218] km/s
+	time of flight: 1.8962639976772875e8 seconds
+	arrival date: 1989-12-27T22:28:57.235
+	thrust profile: [-0.26791212662068803 -0.40688812850114925 0.026691805648649283; -0.266793262589658 -0.3778696834005156 0.027900181098762564; -0.26200529242073944 -0.35378473637283925 0.028633111777203325; -0.25347619440111424 -0.3336772131637166 0.028924627456557037; -0.24128366780550617 -0.3168630085153627 0.02882736146831922; -0.22545597377689272 -0.3028665621167754 0.028380909055401932; -0.20591220119170045 -0.2913793749692859 0.02765148313386833; -0.18239201753865897 -0.2821988061853844 0.026654956702915733; -0.15441194468233171 -0.27517644001068375 0.025384839841290315; -0.12120497217280553 -0.27008163471193997 0.02382575134158362; -0.08180423743214563 -0.26638133593843133 0.021853200343975244; -0.03559861184211625 -0.26289589134190455 0.019323333554878752; 0.01615550067601636 -0.2577838661570208 0.016091495954574812; 0.06905746459059815 -0.2497412095969394 0.012226229591249709; 0.11810325646272977 -0.2395703028520304 0.00804111956320996; 0.16128017869471004 -0.22936084855668964 0.003803922133384859; 0.19913721147690577 -0.22075888291860724 -0.0002865981573597917; 0.23289402715561758 -0.21456195491530816 -0.00412606331776826; 0.2635970662374559 -0.21101943812025215 -0.007646212949431516; 0.29197382006432404 -0.21013550409926826 -0.010839526103107245] %
+Phase 4:
+	Planet: Uranus
+	V∞_in: [-0.6121969849040167, -7.150375871374237, -0.13070109116611242] km/s
+	V∞_out: [0.0007739939100291959, -0.03314950424200176, -7.94754221529655e-5] km/s
+	time of flight: 1.767996002536118e8 seconds
+	arrival date: 1995-08-05T05:28:57.235
+	thrust profile: [0.06556180290998989 -0.4810097896203703 0.001892764138566078; 0.05798846767670954 -0.45547090983767 0.0021156315191879025; 0.051689770885915726 -0.42832132722472177 0.0022959057542090914; 0.04648700280108465 -0.39928121074291384 0.0024336442919551666; 0.0422028841595979 -0.3680710941209755 0.002508087270289503; 0.03867267523413679 -0.3344021401798511 0.002525995849605425; 0.03572097003592147 -0.29802013051252274 0.0024864926364152923; 0.03318882991262833 -0.2587147803564456 0.0023938091349767227; 0.03090542603076421 -0.2163770501304412 0.0022582652803209927; 0.028677181687678518 -0.17104667286314865 0.002097118557040994; 0.02619154533459498 -0.12299356889209265 0.0019574717120907272; 0.022731235300107018 -0.07291026524510676 0.0019498981886554635; 0.013464668655989014 -0.024663380581525153 0.0024792489578653563; 0.022851842286257088 -0.0034654943191003017 -0.0014195501664108637; 0.01695459135761096 0.042960833303929385 0.00027136301763064255; 0.019109715763285105 0.0939108023750647 -0.0006238697198316213; 0.019041699615714294 0.14424641548655956 -0.001297833776791727; 0.0181625271663931 0.1928667562989665 -0.0018850620022324046; 0.016846067007602567 0.23934680582993179 -0.002459940248822858; 0.015214354318562582 0.2834687949061578 -0.003064218239253031] %
+
+Mass Used: 2673.1939593971797 kg
+Launch C3: 43.74597009857089 km²/s²
+||V∞_in||: 7.1777254771611645 km/s

archive/non_saturn/EMJ_2021-10-17T21:08:51.754/mission

@@ -0,0 +1,29 @@
+archive/EMJ_2021-10-17T21:08:51.754/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: 2024-07-06T16:53:06.420
+Launch V∞: [2.823260136727537, 2.381108515747835, -1.1737954184426584] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [2.902861479885485, -0.1301588187286526, 0.5669523646795902] km/s
+	V∞_out: [1.2390632915772526, -2.6409219673539095, 0.5046925355113366] km/s
+	time of flight: 8.406297685905933e7 seconds
+	arrival date: 2027-03-06T15:42:42.420
+	thrust profile: [0.028228817867935244 0.053182566407982926 -0.005054663926030233; 0.005180991851963007 0.0691267924422102 0.013038631124657914; -0.01835805901316754 0.07797668784621446 0.018887537170958094; -0.04313315513357476 0.0809829176156282 0.021806553767181762; -0.06988530553795076 0.07712475685245705 0.02268972139668397; -0.09160758234108493 0.06543179558733468 0.022920454069390864; -0.1098123230541046 0.048341432708635626 0.02151601256114964; -0.12416200616133212 0.027738217207134444 0.020347163167160537; -0.12404293183146138 0.004594899202334194 0.01781507236173057; -0.129155106428887 -0.018581222723093913 0.015298565117590243; -0.12594445263101686 -0.04108652934367247 0.012181435889810483; -0.10860936010879739 -0.05785302549837615 0.00890973312478223; -0.10393797281280423 -0.07897218026647294 0.00494505413203299; -0.08521938934261546 -0.09058792826776481 0.0012801713442578088; -0.06698239018925649 -0.10245050522157627 -0.0027148245589721583; -0.045044579632776124 -0.10478276823574494 -0.006031882980462719; -0.019818627599936134 -0.11139252552545366 -0.010000432210139557; 0.0066242503051877994 -0.10782329745516596 -0.013383858391826825; 0.029766766476497408 -0.09304788741910684 -0.014621131811926025; 0.05750430178483703 -0.08012010231118588 -0.01650664280943883; 0.07827347208136144 -0.05537964439127179 -0.016320867265109163; 0.09261947560772284 -0.02299543299729445 -0.01455858393469228; 0.09914023902019727 0.01591579482167083 -0.011193947076876463; 0.09063940115885241 0.05898855695612724 -0.005929896204151002; 0.06562724891334723 0.09677747829323594 0.0002817010626295331; 0.03846970252523767 0.12968738800889829 0.00626592931214816; -0.014035225318634879 0.1361208554208243 0.01176008272041749; -0.05863663148385729 0.13663351842555724 0.016096346897994468; -0.09798980203153297 0.12317156391252018 0.018711388911181882; -0.1287382519404487 0.10136466288547417 0.020224984128762728; -0.15229270558056937 0.07559496903524954 0.02091790105954753; -0.16565847087960348 0.04430480310028889 0.020006565230859367; -0.17099526669102774 0.011725103749944139 0.017625143996990278; -0.17465152376404056 -0.021415939415702346 0.016435553138393833; -0.1662103957877246 -0.053109462009637225 0.013646899820177756; -0.15857493205251574 -0.0829239406367925 0.01060486274179457; -0.14547673456334026 -0.10870102348055301 0.0070249122604629346; -0.12091234656594241 -0.13188792443501676 0.0032459735017410355; -0.09964673314350471 -0.14990800833225337 -0.0006435420389953807; -0.06918156970036916 -0.16214795228903475 -0.004493281692042949] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [0.9794144953440926, -1.6587037436890903, 0.05654746348233507] km/s
+	V∞_out: [-1.442616061274985, 0.20917386745107652, 0.7533137730861299] km/s
+	time of flight: 2.4817766374856794e8 seconds
+	arrival date: 2035-01-16T01:57:05.420
+	thrust profile: [-0.06322475657399902 -0.4936412371250037 -0.005248083444931861; 0.31392545590226156 -0.5120378343745214 -0.012018965544909697; 0.47194614797631196 -0.3385154091925152 -0.013619738208986319; 0.47127775359634877 -0.06255509378665888 -0.01058423533560999; 0.4308172696537082 0.1701852677638707 -0.006203039675066387; 0.32923840143306177 0.29483054460219477 -0.00246666320173045; 0.18955789797808223 0.3399680173098846 0.0003099824286388989; 0.0431089416132578 0.3578274755748262 0.0018852825335888795; -0.09203547110389645 0.33673084856938534 0.0028123031626823957; -0.19872369663279124 0.30432208370956937 0.005854340007928506; -0.2753934814720275 0.2414543286714742 0.0024528411856131562; -0.31670942879503544 0.16271231757680057 0.002127443207860713; -0.3438228796584529 0.07027601644482545 0.0007277441848606637; -0.3353653444000856 -0.039387445962680574 -0.00019633155682904487; -0.3265117073926918 -0.1386710081315292 -0.001357629546225422; -0.2884243829888734 -0.21671499306159014 -0.0018452201988479967; -0.23036032285216418 -0.2676059176999412 -0.001905654329530745; -0.16057203251898639 -0.300550042644732 -0.0011930641633508003; -0.08352138790234072 -0.31051056059986193 0.00042115538205838047; -0.0031878721141613163 -0.29349054473899483 0.003091115280434996; 0.05993893256943912 -0.26032674719704674 0.0053269904930877045; 0.1034231109686185 -0.22911382612325418 0.008553162275029957; 0.12379922022945494 -0.17899312791607294 0.010143198405040877; 0.12784230457331472 -0.14426714773205093 0.0040528976528373915; 0.12695750648192003 -0.10884078117445839 0.011386843321909838; 0.11632236195028951 -0.07978366535429325 0.011224249977602942; 0.1031692845424281 -0.05338815831167443 0.011316629317471546; 0.09543517501110639 -0.03876712479073331 0.011620292225683908; 0.07781476589416222 -0.023192140146226708 0.01123805571020805; 0.07615001373781183 -0.012209894306577049 0.011721969728096762; 0.06551619304657824 -0.0009017074150139166 0.011163886816134776; 0.053829199564220935 0.009053864413266161 0.010089338822184992; 0.04517243555412592 0.018953951227581048 0.008744400898323478; 0.03335908443255013 0.02708335225021901 0.00691716108064741; 0.022240908301819448 0.03578671309503256 0.004813124702550245; 0.009013884979404078 0.04121040835432829 0.0029897347712111487; -0.002318672961402956 0.04893760947231614 0.00045620814999721825; -0.015217962371449503 0.05539099372635576 -0.002059133107886335; -0.028357882479279055 0.059346949102816016 -0.0037261443912981157; -0.04093441818667926 0.0601240161765365 -0.004707490891211125] %
+
+Mass Used: 587.7637081769217 kg
+Launch C3: 15.018271247758625 km²/s²
+||V∞_in||: 1.927108839335395 km/s

archive/non_saturn/EMJ_2021-10-17T22:10:45.653/mission

@@ -0,0 +1,29 @@
+archive/EMJ_2021-10-17T22:10:45.653/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: 2024-07-11T15:07:13.403
+Launch V∞: [2.955015332011587, 1.7458476003678773, -1.6442790339059827] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [2.777431397042264, -0.6171132169349891, 0.8159382942604554] km/s
+	V∞_out: [0.41916073556198946, -2.93012238170956, -0.008635342159592475] km/s
+	time of flight: 8.130510845924018e7 seconds
+	arrival date: 2027-02-07T15:52:21.403
+	thrust profile: [0.03560871457580073 0.04297807153526013 -0.009741278672567194; 0.010244973922489548 0.0682865729467034 -0.00015039076694469604; -0.01693971645455401 0.07449636960644072 0.004194668780588966; -0.041463139657556526 0.07132437969889172 0.00820671382930803; -0.07040811753124122 0.06106352197572917 0.013202176064717653; -0.08694631593386071 0.049884605249271984 0.019503739077867566; -0.09898847824798032 0.031478229892829834 0.022083102473568192; -0.10895418000615398 0.013676563348540534 0.023302633698378733; -0.12691449163318072 -0.012644795895225745 0.01843151215051371; -0.12045641110596618 -0.02684672402733382 0.017418870855724567; -0.12212419503258157 -0.04673086485788112 0.011086422269240963; -0.1203420954592027 -0.06588801493504692 0.0047685470204244735; -0.05795242400534451 -0.08922342889916524 -0.0004653901145610994; -0.09429663117117613 -0.10154054032347712 -0.005963277296348759; -0.08602550955285351 -0.11155067118451713 -0.012750011019310484; -0.05973099616577391 -0.13049447710772835 -0.012297019716140094; -0.036638352193230674 -0.13245553575387678 -0.01595978207670218; -0.014704821862541679 -0.1322501089295782 -0.017868375747669328; 0.011726912803348645 -0.12879441110498757 -0.021297391177205895; 0.037896798513833124 -0.11110203639268852 -0.020154304305305522; 0.06858668943955744 -0.09088037637425668 -0.01957087600513826; 0.07569655517184265 -0.06833691022819713 -0.017170582433575665; 0.08896168395744229 -0.029932260722520573 -0.015857546505887787; 0.08327090976919839 0.014887707718409622 -0.004674949596662993; 0.0569347369002599 0.05033765253979512 -0.02019213842601755; 0.0438730224167756 0.06178773270046858 -0.009846640656512272; -0.002707912394700384 0.08048933707322277 0.0008223043848798774; -0.027448716543466364 0.0875337570217135 0.010662514924196684; 0.04836017537390385 0.08881272659916994 0.018585019959078204; -0.08418187035941034 0.07571242952898248 0.02342264135972653; -0.10350856671492516 0.06278614246526784 0.026077753064235598; -0.12546895681832662 0.04482241956194045 0.026541904607155095; -0.13677075651969178 0.023070737658912467 0.026394582181228615; -0.14992917554535792 -0.002589877820143231 0.023293165185131557; -0.1555437999314926 -0.029757921489294112 0.019996655414564753; -0.3604924740138941 -0.06775691297914764 0.01618658636296281; -0.11810520991877275 -0.09489413923680597 0.010992192797412103; -0.166979680864926 -0.10172081981146311 0.006460479580690688; -0.11857690368716817 -0.12558680733363264 0.0015917676834061264; -0.0978310318364093 -0.14020655455365144 -0.0033577387161959687] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [0.6909849206531898, -2.478377901106605, 0.14046053907256212] km/s
+	V∞_out: [-1.2244473463866972, -1.7742814019365072, 1.3167491013859527] km/s
+	time of flight: 2.249245348167569e8 seconds
+	arrival date: 2034-03-25T22:54:35.403
+	thrust profile: [-0.15584470628517655 -0.4324448276607902 0.003284332575317339; 0.137053368433428 -0.44929451912740215 -0.008281733610913068; 0.2950039763240335 -0.37465743290758 -0.01440140470924335; 0.34033986005768535 -0.20085030558544617 -0.01798517142849413; 0.38891238354865015 -0.049239121370881024 -0.023461398672222036; 0.30860534743789164 0.07905191176387726 -0.028309665829740933; 0.27349906774928884 0.1645793891956665 -0.03350669968443695; 0.18876993452060792 0.2238437488481321 -0.03809190210228023; 0.07088131458285116 0.26729580185707524 -0.04567869597028036; 0.01712199089749279 0.2758653041516728 -0.043590014047467006; -0.07867139672003513 0.28316801743603404 -0.03710506529649872; -0.16219109103640977 0.2700784539026945 -0.03256498016455749; -0.24485539211217935 0.2587653093997295 -0.02637047963305443; -0.29461607517515004 0.1967042003699304 -0.01937524045582721; -0.36130421453091566 0.11636773623460459 -0.009164784232392628; -0.38731301747903396 0.012976654012294822 -9.942089461904389e-5; -0.36843331546212377 -0.10023886734642075 0.010523932404955257; -0.3553660351889306 -0.2160299060914925 0.020899541778761483; -0.3094574877978442 -0.28306745124739047 0.030274722343385463; -0.2161555591228264 -0.4038330376709315 0.03612257648782955; -0.13965712899980143 -0.3819769536879939 0.04614459131245018; -0.029174136785831986 -0.36487228805316335 0.044897468888315514; 0.07279931081789975 -0.33186898327478137 0.03684689702598207; 0.15279234032190028 -0.30950670474149977 0.01802963641234535; 0.1975684523019069 -0.23293649479847872 -0.00819395847700897; 0.19683722693266403 -0.14283787899855602 -0.031495753711398976; 0.1562485106513122 -0.07724238333698012 -0.03694675816850253; 0.0981433422356431 -0.06618680406669682 -0.016337446005722026; 0.07486247030386232 -0.07170620057618884 0.004115006705080953; 0.059543001830320616 -0.07168192857617524 0.0120096331063191; 0.05458666992894055 -0.06380589771639691 0.0170366352851965; 0.049819955204404 -0.056364543189321194 0.018235897847328923; 0.04376951601267363 -0.046361162805560775 0.01989114609852185; 0.03771044982714965 -0.037432748196631185 0.016269919254059923; 0.03086861381062069 -0.015244554837922376 0.024009666483711486; 0.017344805954934036 0.008486172580677688 0.029915518741446656; -0.004012119607145205 0.0360041583417484 0.025414745902438158; -0.01895134891661821 0.053598270667716434 0.01383046792401079; -0.03887526956647313 0.07298256881732382 -0.010830725775196642; -0.0608588280235995 0.08636421814482291 -0.012419184238920704] %
+
+Mass Used: 556.7628251947933 kg
+Launch C3: 14.483752997476618 km²/s²
+||V∞_in||: 2.576731717563982 km/s

archive/non_saturn/EMJ_2021-10-18T04:47:08.045/mission

@@ -0,0 +1,29 @@
+archive/EMJ_2021-10-18T04:47:08.045/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: 2023-01-22T15:28:09.612
+Launch V∞: [-1.3643798210186435, -0.7159390468343555, -0.08322760218198313] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-3.7275620469034516, -2.526282437303017, -1.0076347004721333] km/s
+	V∞_out: [-4.539673313316336, 0.7017217526549935, -0.43719187658020064] km/s
+	time of flight: 1.6754546939656562e8 seconds
+	arrival date: 2028-05-14T19:52:38.612
+	thrust profile: [-0.07019019845057392 -0.09751722424670824 0.057122211183439194; 0.0054954904966895675 0.06603994792238901 -0.008236600949104998; -0.038287295416854265 0.0405637279948827 -0.00039425725045440414; -0.04489516507237624 0.062361989272701555 -0.014310337466940538; -0.06533576563765808 0.0813139155665736 -0.0230878905705352; -0.07111179879293159 0.1136744968920041 -0.025657586886562084; -0.09903331758106965 0.11244239131194846 -0.029127942276517004; -0.14519955701401654 0.0820620937929571 -0.016479200095645914; -0.18464482626947132 -0.002361270059995381 0.012541372152332043; -0.16208337606711581 -0.12323706727087957 0.029918207581927286; -0.03826611266033134 -0.19280232075714435 0.015634696312891595; 0.10357151304792918 -0.14622474430228383 -0.01476181218722382; 0.16353773698290058 -0.012783112362057128 -0.03817028509721126; 0.14128851582232346 0.10785344001133187 -0.0357190663988926; 0.06918734758690485 0.17326897933390278 -0.03712601380495417; -0.031648944921356836 0.19178367105195807 -0.04461713896061804; -0.12900802224781507 0.16641625303294064 -0.036412410125766376; -0.20558296282247013 0.0909874482041778 -0.0021859875114524693; -0.23860632053617775 -0.03131210259930334 0.03846218187802765; -0.19484928772776763 -0.16847931672520963 0.05663879489729261; -0.04458963976560391 -0.2533559110225395 0.044534431857610954; 0.13733530097702104 -0.21727091374495844 0.020002959834639213; 0.22581551276364645 -0.0879818903955467 -0.0036011782553634036; 0.22121852023447833 0.06669091700849566 -0.01880622457636459; 0.16083994824272446 0.18238419398417918 -0.03735147197382809; 0.04998538539174665 0.24212585751273832 -0.052091359689029074; -0.08535491831784932 0.25306430274112096 -0.05370930001232357; -0.20801975657401187 0.20198148753334175 -0.03429289132017696; -0.29693024644822513 0.07445503890760441 0.00618198553945368; -0.32253861894745967 -0.09834987569122858 0.04557997039335986; -0.23065143773754027 -0.2605588198318397 0.06774871350662658; -0.028464246178048404 -0.33502116968411816 0.0636187256733626; 0.16582275111214603 -0.2932667678437133 0.05643822924252577; 0.2672257697058423 -0.17437196323840912 0.04105153452041249; 0.29453382682696283 -0.016659028012792725 0.025373227704684264; 0.2744616051247645 0.1337722420145339 0.00680861610352153; 0.21887396658872654 0.24585537508513813 -0.014059142888279948; 0.12185436628160583 0.3150537318914091 -0.03596713912282804; -0.033268018178755306 0.3424760568989831 -0.05645515510274152; -0.23160537414128402 0.3196731855067364 -0.06654084457034629] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-1.4846886334994476, -1.361076096805199, 0.05466909001856985] km/s
+	V∞_out: [-0.07465493192041184, 0.9283413652878699, -0.004041543084996275] km/s
+	time of flight: 1.5092081191662246e8 seconds
+	arrival date: 2033-02-24T14:19:29.612
+	thrust profile: [-0.4535229684089248 0.35471159327155716 -0.0057850436284287; -0.5352374523210783 0.14944138395317494 -0.0029283222034505404; -0.520203501923174 -0.06176801084644443 -0.0001628737762102747; -0.5154513050657218 -0.23622401286983016 0.0025982943066399037; -0.46036154582848055 -0.34805331067818845 0.005118780974401044; -0.3959325088841016 -0.41028811107419055 0.0073409773026779646; -0.3235211652890271 -0.4441368112979632 0.009510224295634622; -0.25142435509239425 -0.4658984105671444 0.010858708474655216; -0.18119810986710946 -0.4751147453185688 0.011809185294244101; -0.11638604556530519 -0.47795070872879025 0.012081338602265604; -0.05815970358961853 -0.4728478782242188 0.009857285512696764; -0.00752295071964518 -0.4658771440630143 0.011584161063256278; 0.03545750938514277 -0.4579584297431292 0.010525899201687835; 0.07182273769651207 -0.43472741327897585 0.009533470456107824; 0.10664962568152683 -0.4187208852733485 0.007976992373517903; 0.12492727342133673 -0.3969076832621358 0.006742722154267496; 0.1431746464209061 -0.3835148744685672 0.004786582532343347; 0.1582260654641431 -0.35666588691287027 0.0030847669308384337; 0.16591018189104523 -0.3331316195175424 0.0012721008318001433; 0.17442723323913162 -0.307967948961363 -6.981549779719113e-5; 0.15132680107932436 -0.28549976037098757 -0.0018690202925421497; 0.186781574882658 -0.3306637512391842 -0.0048883590949999976; 0.17610257439350285 -0.23735446317629183 -0.006122412880973916; 0.1724622886167947 -0.21320269056261854 -0.007715271932459695; 0.1680670084063633 -0.19183024967809073 -0.009166796400500983; 0.17830509608470782 -0.16313804745160612 -0.011148105442551353; 0.1482021231934022 -0.14960161104601993 -0.011795475999042142; 0.14034852593908412 -0.12424858172274011 -0.01351806966068364; 0.12814622777773102 -0.11065483266711279 -0.014425856538434116; 0.11336824983566328 -0.09468285579432549 -0.015153154561936515; 0.1014135174333853 -0.07774054155124342 -0.01636862595604425; 0.09013879877718133 -0.06314251860721383 -0.017328209330542098; 0.07409816899410408 -0.04958972068223582 -0.017982560903710178; 0.059254084971633196 -0.037404541491299056 -0.018443983864669375; 0.04564010326731609 -0.02708329971030048 -0.01901529707592924; 0.031119604581005364 -0.013731126495017738 -0.0194930452946951; 0.01819976084858475 -0.010230335153065933 -0.01913899819718352; 0.004680675542116217 -0.0019477725404852817 -0.018630645585022216; -0.006945877458896208 0.04945640047608528 -0.019980625053223188; -0.02476220854549837 0.020757355899770503 -0.018288826690161054] %
+
+Mass Used: 699.0068365759485 kg
+Launch C3: 2.3810278485499135 km²/s²
+||V∞_in||: 2.014898803697196 km/s

archive/non_saturn/EMJ_2021-10-18T05:50:38.255/mission

@@ -0,0 +1,29 @@
+archive/EMJ_2021-10-18T05:50:38.255/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: 2023-02-05T01:45:05.243
+Launch V∞: [-3.0858219124135338, -1.9843415638102107, -0.5164890400755199] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-4.057237445286011, -4.383306689219025, -0.9345749583183188] km/s
+	V∞_out: [-5.708063773850215, -1.9703162053834726, -0.2898885846278176] km/s
+	time of flight: 1.7154989176181787e8 seconds
+	arrival date: 2028-07-13T14:29:56.243
+	thrust profile: [-0.05903412749179622 -0.11072573240494099 -0.046313134098117194; 0.01830167102423096 -0.06087146903047021 -0.033049847954461684; 0.07560298617807773 -0.01056944361432975 -0.028709358840799726; 0.09546806703287268 0.03818316915239496 -0.01815506148240239; 0.087072908846325 0.08753619540094806 -0.010262863619545785; 0.07369552306131616 0.12499222126459184 -0.006697651325533921; 0.04251662528606648 0.15925223632421193 -0.004792029859755092; -0.010226965163121535 0.17556129615047028 -0.003737106470399883; -0.07525867128506282 0.17117299059876928 -0.0026437347892256744; -0.1429171951031634 0.13309299620733395 0.0009660268333295966; -0.17674866813873913 0.04237741241467234 0.011493155256722482; -0.1512076116827121 -0.08040347524944479 0.02330619578530688; -0.05115883020169031 -0.14141553541705287 0.017131006896436887; 0.05087583129540856 -0.1315744035343398 0.010336510514475119; 0.1120126200517782 -0.0799539576707552 0.002371562967016136; 0.1443467696695813 -0.018236726608329784 -0.004456458124353138; 0.15584788026095098 0.051389436140585935 -0.008686824078125708; 0.14558302648535318 0.11755108446303067 -0.010892189302993153; 0.11394327968434129 0.17080316758040615 -0.012668785007190191; 0.06296089219227079 0.21032613587651547 -0.014424861687090097; -0.007319181749241606 0.23302483496293394 -0.015775127894478227; -0.09208540070014654 0.23384051362199884 -0.016036796645284054; -0.17801224449074027 0.1988282553478485 -0.013451405628367928; -0.2405987292175941 0.11053687540893897 -0.0037755605782861168; -0.26274834968674954 -0.03215539584325131 0.011401533519479992; -0.18944534529519497 -0.16935814231584914 0.023680470151096394; -0.062492398971191944 -0.226809847819523 0.025148014577392675; 0.058741104153245675 -0.20710110554056518 0.02325277700839408; 0.13496703268042476 -0.14953850565375484 0.02002722387428528; 0.17788592589491933 -0.0842582776450467 0.01576195229274432; 0.2134153344492731 -0.01219022142044608 0.011716260687670104; 0.221133806934409 0.06664309280990648 0.009067992486418756; 0.20670820225401887 0.13977111236609446 0.007216324831558612; 0.17685233175682644 0.2009155862624451 0.004901929518232841; 0.13210453725383495 0.25576220417288764 0.0019161352306033082; 0.06729420380240994 0.30354914394899996 -0.0015851356597052838; -0.021728498222142328 0.31746498514577615 -0.006950254934209666; -0.12282179274563348 0.31897417027587177 -0.01342616228297283; -0.22216672837379955 0.28264007424096826 -0.021319790289976142; -0.3061983927615912 0.20656298357463285 -0.02872946037718458] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-3.099527737126561, -0.7982552067237872, 0.5013266698433383] km/s
+	V∞_out: [0.041592732646317895, 1.627725242681464, 1.3244467950891392] km/s
+	time of flight: 1.2785674190820272e8 seconds
+	arrival date: 2032-08-01T10:15:37.243
+	thrust profile: [-0.41604742347230705 0.06737894984312282 -0.04205491392883786; -0.3861211958007792 -0.0758091335673133 -0.05360756017666809; -0.38159338209724647 -0.18683783846640528 -0.060539772129709346; -0.3350949731987023 -0.2563119526230099 -0.06133971353596192; -0.2871521785597488 -0.32348412532931814 -0.05786399726102912; -0.22253747113558456 -0.3141454362424642 -0.05305353968999086; -0.1648658017684768 -0.29697975715716984 -0.04751117142541355; -0.12442069988353341 -0.3116638659514345 -0.038228092969129816; -0.08111462090829119 -0.3069867266716785 -0.029740118494018575; -0.04613498335535642 -0.2951117896245657 -0.021059313316040384; -0.018598978169875633 -0.2815182543648192 -0.012932002016639724; 0.0045256419165849065 -0.2669272627444781 -0.004427429319138051; 0.0234811875972447 -0.25209972076750015 0.0029723567713946576; 0.039274945308955506 -0.24056465141722116 0.00993362495845694; 0.051426343418473616 -0.22281194727419235 0.016345479125692383; 0.06086343873321743 -0.2081388161322731 0.02188664991008354; 0.0685065126238841 -0.1926572918357054 0.026839097522788475; 0.07525744827143042 -0.18093945742485354 0.031075223064810226; 0.079392823582722 -0.16606035049084994 0.03454357195394954; 0.08295943887786963 -0.15412750790018656 0.03740347939202216; 0.08613999214593006 -0.1428938322974369 0.0395012677076581; 0.08772834490249906 -0.1310169948154417 0.04092188439412888; 0.08895334110394983 -0.1202339756399574 0.041849591117764914; 0.08730997577811128 -0.10626040353133856 0.04252301660314416; 0.08869148570645749 -0.09867056588432131 0.04236667383009366; 0.08803735659001409 -0.08883483723685866 0.0409433140159136; 0.08655169773377087 -0.07939821085862654 0.039500208451252544; 0.08531407495440747 -0.07069193052001756 0.037483909758018345; 0.0839157998172722 -0.06262433392398156 0.03491784670387027; 0.08241104639095365 -0.05456127680876876 0.031905310581824844; 0.08029247052881323 -0.047080198594668 0.028489062021749233; 0.07785957445382675 -0.039291190198784826 0.02477996888593748; 0.0764785313388362 -0.03234957407371497 0.020441460714379626; 0.07364576084853765 -0.02495977005348136 0.016149035754968472; 0.07045328958061775 -0.01772137162673052 0.011686575379395969; 0.0683660123350372 -0.010636482284919705 0.006942049179465146; 0.06625158462271445 -0.0033382009537524177 0.0022901113272747508; 0.06165831780883017 0.004819216901214894 -0.0015177666265392743; 0.05770562649405053 0.012951600227321435 -0.003618598699498523; 0.05264085001752809 0.021136344288158682 -0.003411686116928844] %
+
+Mass Used: 495.9436459575345 kg
+Launch C3: 13.726669245514401 km²/s²
+||V∞_in||: 3.239693195068747 km/s

archive/non_saturn/EMJ_2021-11-07T15:15:24.057/mission

@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMJ_2021-11-07T15:15:24.057/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2023-01-23T13:44:20.247
+Launch V∞: [-0.1739597247433209, -1.5392251924256757, 0.1510741902051145] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-1.747388916324353, -2.061505608833443, 0.004246536679567164] km/s
+	V∞_out: [-2.4403954507440164, -1.1573303397285044, 0.09102116739890352] km/s
+	time of flight: 1.0791720765728353e8 seconds
+	arrival date: 2026-06-25T14:44:27.247
+	thrust profile: [-0.003437324500446065 -0.06316993477714959 -0.03227448158061817; 0.01567838811254846 -0.026330238009065726 -0.042075545977590216; 0.05142670882061399 0.03192109164526059 -0.030663473328706496; 0.18494150891704356 -0.05996396933783311 0.07272546357288993; 0.01987844881950037 -0.08012428438452728 0.14827651870110511; 0.0478009970849944 -0.02735889058433289 0.07798896298034431; -0.04075898555607768 0.11085612294078731 0.04603514580947307; -0.13952989202410981 -0.056985214724475576 -0.027200205223449195; 0.08522507291755119 -0.062139974359961894 -0.07129854782691303; 0.05351401270498842 -0.015500763055453866 -0.05259023429164523; 0.011282221363737887 0.02079500823213104 0.022523283753477914; 0.000699535966496786 0.09778479936527512 0.046529957624245714; -0.1030612853651482 0.12427737748752737 0.06708573684290235; -0.2038465893015885 0.014273665407528257 0.03802819777346354; -0.15618783028550054 -0.22318260536732798 -0.03742174282404114; 0.11410391007602544 -0.2082315215516395 -0.07040126308718953; 0.2521672881323561 -0.03769876422261141 -0.071688270611509; 0.23266831751793693 0.18743463203159552 -0.04551839351936565; 0.11519460197453685 0.3302484081094953 -0.02252892387897748; -0.18122294990431062 0.36229081369121324 0.04269874956058407] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-6.804956827112563, -4.679824047197812, 0.07151821136919514] km/s
+	V∞_out: [-0.032527135720069, 0.001544851923976201, -0.00019858586424769518] km/s
+	time of flight: 1.3383000099773991e8 seconds
+	arrival date: 2030-09-21T13:44:27.247
+	thrust profile: [-0.1392065495307979 0.004750835268938231 0.023507505308300022; -0.19310508213400865 -0.033187172798787246 0.03720253217974291; -0.08401649310562243 -0.03721535067081677 0.018686610849057983; -0.07189175926991606 -0.010086246689719958 0.002137809069141927; -0.04577388220162917 0.041578634569519 -0.018853960583673845; -0.1661362264023361 0.06506520619848838 -0.009449430204867661; -0.19796870421884868 0.04783193521476848 -0.023213922479647067; -0.12983109381999572 0.047003643397231905 -0.03086558152561419; -0.0882948553314463 0.1475664155854163 -0.017260515869025956; -0.3366163399243817 0.39553588365930525 0.015795560486203543; -0.640980062057629 0.2632981931405252 0.0812643122284222; -0.6170331837293128 -0.3303891659922319 0.08145169051162247; -0.417277476379212 -0.4064979390965165 0.057948112978786846; -0.1920015280971652 -0.28614848876207744 0.021902037419699424; -0.04488825027754133 -0.07688374836411227 -0.0050070954905793545; -0.020349917091670125 -0.03323033529641674 -0.02767377795875804; 0.0034924766822311388 -0.014218666042869754 0.006356643814839159; 0.00039701408140195273 -0.023899377007047005 0.09028397293070597; 0.052254845117264026 0.028631960813363038 0.004727246748924411; 0.03093967952976618 0.02034528891395188 -0.008818558262886378] %
+
+Mass Used: 1779.3184287128902 kg
+Launch C3: 2.422299589776762 km²/s²
+||V∞_in||: 8.259134663277639 km/s

archive/non_saturn/EMJ_2021-11-07T16:44:24.602/mission

@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMJ_2021-11-07T16:44:24.602/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2027-07-20T13:17:34.631
+Launch V∞: [-2.3530089890058954, 1.806546373465246, -0.8246183971035168] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-3.557079179490031, 2.2348168420384456, 1.4054671292663363] km/s
+	V∞_out: [-4.074087303045588, -1.0849670349142753, 1.3593729379381074] km/s
+	time of flight: 1.0695600026560412e8 seconds
+	arrival date: 2030-12-09T11:17:34.631
+	thrust profile: [-0.0022189023782523748 0.023365002143236557 -0.010993409331132617; 0.2153019288203301 -0.16440845543934793 0.012979033551565024; 0.3639464079118591 0.18422132432552532 0.04272023217963688; 0.11466184077416293 0.3079055688420129 0.008827434981649196; 0.030850502559811713 0.10710583581109685 -0.0392443866311469; 0.12842405226198722 0.13471500586493157 -0.046470788171139685; 0.022178550605493758 0.08362899413062866 0.012804941168562645; 0.12528977866442487 0.07930598418341506 0.05523752701719965; 0.11036663197880708 0.06908833586375046 0.030544670010797404; 0.2621885557666051 0.017745488649470693 -0.043256804103609825; 0.32712194273437595 0.3540199595758462 -0.06793264883835635; -0.12456921081136497 0.30022659769281007 0.011877569185517847; -0.111118550048934 -0.0012849144456734945 0.0618346466936284; 0.0664475480767869 -0.20857672555247925 0.05232162118008461; 0.4674741919141163 -0.27665818135554127 -0.010294403145171388; 0.6235722276862998 0.33893717906065446 -0.08396785235072478; 0.06141376840855648 0.6645340284197009 -0.04540915059549516; -0.4950753135059394 0.4265532645880646 0.04403645965499313; -0.4790065958792388 -0.05470792785400573 0.08950665085522541; -0.31489858710635427 -0.3741453611976776 0.10307557908026614] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [0.38917010093640664, -4.172653280725571, -0.38172849726338637] km/s
+	V∞_out: [-0.19079117316696953, -0.697272265566823, -3.556895184028567] km/s
+	time of flight: 9.204480003834815e7 seconds
+	arrival date: 2033-11-08T19:17:34.631
+	thrust profile: [-0.28696988915862254 -0.5466775279353076 0.0161784825048141; -0.05201138624094085 -0.5103548545163037 0.022399691416144073; 0.09258223397854948 -0.42700369632306956 0.02864531312701303; 0.1544195747765251 -0.3175042943871396 0.03319962132309101; 0.16629852231537434 -0.20372710365454566 0.033385847516108444; 0.14766618426707362 -0.10862149045095645 0.026893053884926972; 0.10680433249395786 -0.047590669692367006 0.013917994143247845; 0.05372607652222386 -0.024738666039118885 0.004540404069389168; 0.0454652164291245 -0.03203318353562152 0.003800593821863827; 0.06019445610850742 -0.07020561382583693 -0.0007266034614935319; 0.031747954241254955 -0.05399780408669305 0.0026705429420879126; 0.008868957922568855 -0.0550458335463559 0.003204913050222715; -0.0001325460641792178 -0.0009815769471698307 -0.0004937922234238575; -0.0006857531267272214 -0.007291536557149579 -0.0032616756502396376; -0.002795903533707593 -0.01051173235400901 -0.00025468873326567386; -0.0011701726557658773 0.007181885264360277 0.019496153473968613; -0.00244282675331443 -0.004315368336196475 -0.00303667834001964; -0.005725948352347262 -0.005635872428339283 -0.003961276803316091; -0.017216802798993906 -0.013717525082576966 -0.016160860429875766; -0.026100664086817275 -0.009712024123055465 -0.043657502180151124] %
+
+Mass Used: 1804.5751392877032 kg
+Launch C3: 9.48025660266455 km²/s²
+||V∞_in||: 4.208111858569789 km/s

archive/non_saturn/EMMJ_2021-11-07T16:11:36.123/mission

@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMMJ_2021-11-07T16:11:36.123/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2023-10-04T23:54:18.571
+Launch V∞: [-1.0946372744813206, 1.772856344640237, 0.6518921748479192] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-2.468570935539311, 3.9145499143885183, 0.294185580247984] km/s
+	V∞_out: [-1.0716225311162524, 3.7979475765527537, 2.433225426462671] km/s
+	time of flight: 5.03315786710681e7 seconds
+	arrival date: 2025-05-09T12:53:56.571
+	thrust profile: [0.05761170096388485 0.0037768374968660183 0.021446902745431394; 0.2338910222642935 0.038442540157432946 0.07384370283448043; 0.3763154163892285 0.15798877805762376 0.10760306536830927; 0.44522680521020497 0.3325874829511538 0.12042194905157132; 0.43452219983563223 0.4761595527593114 0.112248412068997; 0.35455482283622286 0.5534063389960954 0.08620789727452381; 0.22637206987130523 0.5641403611112387 0.047320282881539735; 0.10563883830837441 0.5173755101163249 0.0020211160360646316; 0.08552855616331344 0.4304437643000631 -0.04218486298987761; 0.1960853756766005 0.3596225932161036 -0.07804050817173727; 0.36832809338191125 0.41628231583740644 -0.10121628933922924; 0.4357323056908466 0.5885680060443318 -0.08777037764641167; 0.19220878836448985 0.6988618533998787 -0.02928321108356858; -0.3260372445818445 0.6741273897794257 0.04276866734928403; -0.4765259655030003 0.5334483571862702 0.09600999744682062; -0.43336445416827124 0.32586427042694366 0.11746957265742869; -0.3020278694727908 0.14307106565129288 0.11022531383572896; -0.13802052724283995 0.0283940948753469 0.07716223945632268; 0.000379994255704275 -0.02970595003409978 0.00908639547659395; -0.008600438414250629 -0.00609678077148597 -0.0010028719112170669] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [-2.4967999712121305, 1.1505263293360948, 2.948442751619554] km/s
+	V∞_out: [-3.1906741181460436, -1.6861119385410752, 1.8063767169662492] km/s
+	time of flight: 1.733327609059168e8 seconds
+	arrival date: 2030-11-05T16:53:16.571
+	thrust profile: [-0.0017142861123577843 -0.007699559345150912 -0.006388535937084047; 0.017904027729335064 -0.010463864728501053 -0.012211253494710993; -0.11452589870067577 -0.22152358678387732 -0.0210809740841956; 0.01156443159091045 -0.003897368532065136 0.004479440617280323; -0.0018576450376501718 -0.0007623677091815274 0.0017808732034867247; 0.009993325332786733 0.0014150710040253416 -0.000512307205177813; 0.002647239103741267 -0.0013242606436760882 -0.004976891838670212; 0.014924541796774602 0.0037605945568966142 0.009596392756040205; -0.017618584749391118 -0.017529516289992483 0.019033520509682534; -0.026042865995432426 -0.0865312956614177 -0.011374581928173356; 0.052154252911354115 -0.13213003153993366 -0.05375112701888339; 0.0020590554705049204 0.01030638727355359 -0.0016438826565531737; -0.00014214150335625986 0.0033114821791039133 0.006549338245203575; -0.07377901396357853 -0.03027409142259342 0.03084760058305368; -0.06206451078100525 -0.3063894058582564 0.005825322685388118; 0.17699628309895177 -0.3111676416860315 -0.10663911315716215; 0.05964752199148081 -0.005831291932262422 -0.04999533519370418; -0.004431558848567231 0.007860815818719002 0.0013374590748647765; -0.15456383911087573 0.028309448158751086 0.11359293087912255; -0.39271294367560633 -0.29698573943715145 0.17818484103244142] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [1.4924422600995255, -5.560592732188845, -0.4685665727537283] km/s
+	V∞_out: [0.2666192989414379, -0.035476903402614585, 0.4252672489349129] km/s
+	time of flight: 7.801559990038186e7 seconds
+	arrival date: 2033-04-26T15:53:15.571
+	thrust profile: [-0.05667547933380966 -0.34967018073611944 0.002732189029373461; 0.010392070890743524 -0.38900231469874 0.012454157781016004; 0.09333137039669492 -0.3933837603455368 0.02000090481188271; 0.15503747405291288 -0.3683065023975787 0.025757684941636973; 0.18293674988995412 -0.3205125326753517 0.029768540395580415; 0.17930535445082396 -0.2591475229314961 0.0318370703301853; 0.15076970710143955 -0.19372274550885235 0.03170102566964771; 0.10458817867769576 -0.13175745133709596 0.028987564999421418; 0.04878214365636921 -0.07674432001861356 0.02291451019660362; -0.002030516198702912 -0.02688349362194637 0.011613325437291943; -0.006034286792027756 0.004438215059932985 0.00017918447185226728; 0.005445584386242583 -0.00816473676350179 0.004379586882810379; 0.002909662764884706 0.00012505110525283484 -0.0007139817309227709; -0.002056634454649893 0.0030597981679055665 0.004983246314934733; 0.023984266237933233 0.012127202259832088 0.014123155751866866; 0.015229836090100148 0.0882800459102248 -0.0010477895180961438; 0.02210000369026799 0.014238614166865187 0.005816636018140111; -0.0020399990692374255 0.004805026000813184 -0.0010618970952335149; -0.04612931543476969 -0.0038678412517168994 -0.01979479274534377; -0.0331200841636588 -0.02846676207386028 0.0062777303019229585] %
+
+Mass Used: 1973.258531533688 kg
+Launch C3: 4.766213789042987 km²/s²
+||V∞_in||: 5.776428833293505 km/s

archive/non_saturn/EMMJ_2021-11-07T18:27:10.222/mission

@@ -0,0 +1,36 @@
+/home/connor/projects/thesis/archive/EMMJ_2021-11-07T18:27:10.222/mission---------------------------
+
+Spacecraft: bepi
+	dry_mass: 2000.0 kg
+	specific impulse: 2800.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 0.9
+Launch Mass: 4000.0 kg
+Launch Date: 2027-02-01T18:33:11.110
+Launch V∞: [-3.150497013090804, -2.3173169584138944, 0.341495631383101] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.7086971873088551, -0.10655494257324054, 0.11988806590713104] km/s
+	V∞_out: [0.2238809651804253, -0.3118676174457644, 0.6168980985050387] km/s
+	time of flight: 8.953200023401788e7 seconds
+	arrival date: 2029-12-04T00:33:11.110
+	thrust profile: [-0.12186870505136849 0.09462644883825748 -0.05810534392839175; -0.030639242847821345 -0.04245910692035197 -0.0894052455624086; 0.14113718480937812 -0.11440231644835337 -0.08324956933880284; 0.2837902510213314 -0.06260096981677356 -0.0550413035881179; 0.35855908041409906 0.04073648975482989 -0.020180975564470557; 0.3729359388901653 0.15239321939968276 0.016136485697739962; 0.3362801729367708 0.23639200487749643 0.047870876871699004; 0.26251183204522277 0.2735012454673692 0.06987761022138216; 0.17815253145241594 0.2588190065709617 0.07748014522346204; 0.11663205314604401 0.2103183053176405 0.07202476138100809; 0.11053399149833462 0.17008886355865674 0.06219240053201351; 0.16138151083151792 0.16508258430710807 0.0517839189038665; 0.21005359977761767 0.21368458752750677 0.0315693543261013; 0.19623229223435448 0.2814455053854785 0.001570447612348246; 0.12163118057275962 0.3027077944605196 -0.0304471015663471; 0.050711982127557564 0.25718214500209285 -0.05394847268359673; 0.02648153137529395 0.16832831911941415 -0.05881608102540833; 0.04710479095848209 0.08697307038303437 -0.03899890258876461; 0.07958628725681302 0.06854595922468731 -0.009001942082726883; 0.08605410384534219 0.09736430380889433 0.020673442685919103] %
+Phase 2:
+	Planet: Mars
+	V∞_in: [-0.86775765928764, 0.239785321439957, -0.2793440299073699] km/s
+	V∞_out: [-0.728269228104112, 0.22205886592425675, -0.5557724748024003] km/s
+	time of flight: 1.9774800534204435e7 seconds
+	arrival date: 2030-07-20T21:33:11.110
+	thrust profile: [-0.030570769176673163 0.011978049730521367 -0.1686311146776997; -0.03734362480961287 0.018449018456192904 -0.17005264964682357; -0.04542948419070008 0.025365372398860525 -0.16992835340263743; -0.05521690145245066 0.03285244672122282 -0.16774923049721527; -0.06706930468913055 0.04078685922552811 -0.16334874802709573; -0.08131104167653695 0.04884139923754264 -0.15672575498494773; -0.09819592248044624 0.05655952543787853 -0.1479650657154312; -0.11787873911002066 0.06337920264640957 -0.13717350608484466; -0.14034999306643528 0.06867765983804668 -0.12442413309677075; -0.16539190427907322 0.07179396518491549 -0.10977409185801229; -0.1925589065058879 0.07205624162537454 -0.09328712290120528; -0.22119886531630267 0.06885264399706031 -0.07507799161161761; -0.2505343015720731 0.061677462874266016 -0.05534950074382844; -0.2797189023307287 0.05017836496163492 -0.03436640779599943; -0.3079203344948388 0.03418116061894368 -0.012445205871944063; -0.334368663091996 0.013690266374333697 0.010060492482634029; -0.35838748770071316 -0.011093871325495122 0.03277754892305918; -0.37942569771654455 -0.039796379505630045 0.055325239511752944; -0.3970806444181828 -0.07189338316019264 0.07733706717380652; -0.4112725932874617 -0.10674559801233943 0.098568724917307] %
+Phase 3:
+	Planet: Jupiter
+	V∞_in: [3.096628165859758, -5.54752603323759, 0.16307349334680107] km/s
+	V∞_out: [-0.10793078996383877, 0.0924800512858945, -0.022459388754450135] km/s
+	time of flight: 8.654760001509127e7 seconds
+	arrival date: 2033-04-17T14:33:11.110
+	thrust profile: [-0.5212124178884477 -0.24272925296458728 0.016173224831160182; -0.48041901371361273 -0.42824969367860183 0.03503551018937675; -0.35657251411134105 -0.5210283603639988 0.03882674235576436; -0.18159148927663898 -0.5413874907790582 0.03142458257784628; -0.021760680952925514 -0.5187437230839083 0.020044129391221313; 0.08815802808124944 -0.468755585771906 0.008811701650286144; 0.14996577274874454 -0.39950153509190717 -0.0006374540546909846; 0.1756826332108901 -0.31843613205645516 -0.007389149611688129; 0.17606438164463012 -0.23381194273364414 -0.01163475824093298; 0.159181144560096 -0.15334688886711978 -0.013041705195263514; 0.13078599845765138 -0.08380131179134265 -0.011046703931163082; 0.09565122980609836 -0.03262766659535713 -0.006008779003864255; 0.06498733257355833 -0.009875081025971531 -0.0018112250669574325; 0.057070637186324664 -0.005117739296306144 -0.0016028113399474964; 0.06624558635734848 0.0072126749803919175 -0.0040159232988713255; 0.05783875168815469 0.01498693837279799 -0.003335562522287042; 0.04729181899024323 0.02021996828138974 -0.0030204665772785907; 0.057434402651546965 0.035842653333588784 -0.00310080378363583; 0.053208582397478485 0.046380716067435886 -0.0063431045982933485; 0.02806058144310276 0.03766447626177584 -0.005388583041760812] %
+
+Mass Used: 1879.386292887199 kg
+Launch C3: 15.412208581500444 km²/s²
+||V∞_in||: 6.355371275643704 km/s

archive/non_saturn/EMN_2021-10-15T14:10:16.844/mission

@@ -0,0 +1,29 @@
+archive/EMN_2021-10-15T14:10:16.844/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: 2022-06-15T03:21:18.518
+Launch V∞: [0.048117896423172386, -0.5162092686244537, 0.40407035227141913] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.9344418663833501, -1.94113411605789, -1.3161154740790337] km/s
+	V∞_out: [-2.14211756398572, 0.9624191156710435, -0.9264823839100106] km/s
+	time of flight: 1.2644457083492844e8 seconds
+	arrival date: 2026-06-17T14:50:48.518
+	thrust profile: [-0.10448028441523405 -0.1256907202270118 -0.16091866640079286; -0.19904783374877122 0.10871884567825597 -0.1306688148649953; -0.19709408994597308 -0.1674300798982282 0.005069018791283623; -0.004291263269297833 -0.399104721177389 0.09790570282026163; 0.29748596325897214 -0.19017236336276858 0.06829748140772242; 0.18208731695990318 0.19543127312804398 -0.1515167603279824; -0.147097144668956 0.26471504859691886 -0.12993685282980716; -0.3254377977798237 -0.07921471871314706 -0.013320620685086488; -0.18111215875786393 -0.3419227077323917 0.07609889998875147; 0.23174255714522965 -0.32712228294832624 0.06447883065044928; 0.6721056690892853 -0.02043336602254751 -0.010181899875232497; 0.22228391170390308 0.2855335978224687 -0.10159902960358226; -0.168431496892007 0.30418945279932713 -0.070730113166975; -0.32913534843792436 -0.00484741033042222 -0.008166308801170486; -0.26947039532575157 -0.28510731387791954 0.07359876392089902; 0.05790671500570107 -0.3802998506280197 0.0866314905921983; 0.26049733990679225 -0.28812017972418896 0.01928824704441663; 0.40015076156150897 -0.011025507485978085 -0.057150879950288155; 0.20552272464587207 0.21210558478528038 -0.108254263904822; -0.0647634110268568 0.24072563384380027 -0.05160771738920396] %
+Phase 2:
+	Planet: Neptune
+	V∞_in: [2.828147217989047, 0.7175168734464545, 1.0176840385312307] km/s
+	V∞_out: [3.088960098692494, 0.0009651340319555146, 0.0070539549539161365] km/s
+	time of flight: 3.697305578398602e8 seconds
+	arrival date: 2038-03-05T21:46:45.518
+	thrust profile: [-0.682488113771849 0.13920676013767327 0.13229199047890008; -0.3820716934910725 -0.6941984698101173 0.012657220760168286; 0.5853107150693558 -0.6317019149478917 -0.02534339780785512; 0.6740197859912153 -0.5324864753684241 -0.06972765095384162; 0.6868798169923216 -0.222502142017196 -0.0661829601036205; 0.6280074153513623 0.12208601430674178 -0.08384824254232823; 0.6143769984593854 0.19563277757575892 -0.05047133576620455; 0.5240798395183139 0.21175930544481952 -0.029002996472197947; 0.443569382057989 0.20852765023008743 -0.02019580607789296; 0.4131293690460721 0.18484645183186532 -0.043147082866315294; 0.3421032285788577 0.17265685215195495 -0.04625167892683922; 0.31496404643914705 0.09909975530478392 -0.032788142105343726; 0.25985581121428897 0.07020561472862764 -0.016911332791942423; -0.132085517447492 -0.04615718911621035 0.13481526251714143; -0.25767269995543396 -0.09890431522085448 0.08074154160499622; -0.32635582434111154 -0.1543465615608083 0.053298387650411234; -0.3800377852121974 -0.17219786514243648 0.04605792593383556; -0.45767813054385165 -0.19901912427065352 0.045668370100405344; -0.49742956858989346 -0.21654911975942986 0.04409302561596516; -0.6018269818439854 -0.2341358293674843 0.018963648582648505] %
+
+Mass Used: 1936.6395511020824 kg
+Launch C3: 0.4320601905547333 km²/s²
+||V∞_in||: 3.090133970005313 km/s

archive/non_saturn/EN_2021-10-14T21:24:00.053/mission

@@ -0,0 +1,22 @@
+archive/EN_2021-10-14T21:24:00.053/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 1.0
+Launch Mass: 2500.0 kg
+Launch Date: 2022-08-05T13:09:42.428
+Launch V∞: [7.8646219457877775, 5.391423246731976, 0.21664193585734026] km/s
+Phase 1:
+	Planet: Neptune
+	V∞_in: [4.3825277514495635, 0.4972219444711066, -0.033282491583832376] km/s
+	V∞_out: [1.2613145775799692, 1.2541088206742887, 1.19448213244607] km/s
+	time of flight: 7.239210268385214e7 seconds
+	arrival date: 2024-11-20T10:04:44.428
+	thrust profile: [0.5570971125040689 0.46523336275569166 0.24443397992833363; 0.5455353078277998 0.37771233171043145 -0.2905042836424388; 0.5373067044309571 -0.3697335845815613 -0.23280971000434258; 0.5789141430780081 -0.4290239526125613 0.17533812742230417; 0.6282895761794832 -0.4760003782283056 -0.02869288371312378; 0.5937505020656196 -0.44907996753558815 0.008871484612811375; 0.583505825104241 -0.4419058605742258 0.0024181680115527163; 0.5999629018966298 -0.4488350427074705 -0.0010636832749702108; 0.6282809657618084 -0.4727189600895791 -0.0029164733714258264; 0.6387620784811242 -0.4812400030251487 -0.004086578863408878; 0.6291065200722094 -0.4782777977932136 -0.004926811268235369; 0.6685784074664406 -0.5147308829624088 -0.005566898376192713; 0.6402182196889159 -0.4886680265057143 -0.005534056457267186; 0.7138116778721744 -0.5642610603445648 -0.006396711596120154; 0.6435783521271209 -0.5330961196095906 -0.005999671526644724; 0.596620975387932 -0.5192282791418487 -0.005575460237394601; 0.5813910956156 -0.5172814194247172 -0.00522147564686555; 0.6107615648872227 -0.524352387609911 -0.0051458063628017055; 0.6046402368385538 -0.4209917190545011 -0.005257320993026065; -0.23129745811295646 -0.24034385286604382 0.002372195721427373] %
+
+Mass Used: 1747.3636846345928 kg
+Launch C3: 90.9666567039407 km²/s²
+||V∞_in||: 4.4107694202412375 km/s

archive/non_saturn/EN_2021-10-14T22:19:11.393/mission

@@ -0,0 +1,22 @@
+archive/EN_2021-10-14T22:19:11.393/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: 2022-04-16T10:37:51.889
+Launch V∞: [9.93430356594082, -9.814231711705617, -9.723022803164637] km/s
+Phase 1:
+	Planet: Neptune
+	V∞_in: [-3.330351073892173, -5.42324969269204, 0.08855958401956425] km/s
+	V∞_out: [-3.300747312670549, -3.328777757532345, 3.3127008443655095] km/s
+	time of flight: 1.007092354462312e8 seconds
+	arrival date: 2025-06-25T01:25:06.889
+	thrust profile: [0.8753926904953222 0.6832826274506226 -0.12190291359862054; 0.8755956380471712 0.6667237002096869 -0.1464038516358984; 0.8745742225785343 0.5149107423186586 -0.17002603241860648; 0.8637408209307073 0.25941037509054327 -0.19687061798657313; 0.8873044529895101 -0.013949833656543549 -0.20801896083211308; 0.8603140096952885 -0.22178564312493226 -0.21226327319113722; 0.8722049558724008 -0.35639346957623513 -0.20814872623709274; 0.8798839779340266 -0.4459725813099044 -0.2408854578792029; 0.8297808636995301 -0.4620621965066881 -0.1882977763047611; 0.860562943045671 -0.48184951051800107 -0.19082816411413117; 0.8605004943271973 -0.44955972119045773 -0.19270354692519773; 0.8747678471057356 -0.47094234663449625 -0.19348022139751583; 0.8729759234509828 -0.47846767255653266 -0.1955394172393871; 0.8588899256657108 -0.4743430479827928 -0.18332350007377493; 0.8588081308592396 -0.46834855863482244 -0.18530291711509578; 0.9286451187684647 -0.4728485531364328 -0.24687867162402924; 0.8722317541853327 -0.472450161676079 -0.21522005038654823; 0.8290733251430757 0.6523310686037682 -0.0183400190880806; 0.8629624567917368 0.9173769916931223 -0.01773284000590214; 0.8426122479515165 0.860803708329764 -0.020651982695331434] %
+
+Mass Used: 825.0187357617949 kg
+Launch C3: 289.5467038621722 km²/s²
+||V∞_in||: 6.364803084509432 km/s

archive/non_saturn/EN_2021-10-14T23:27:47/mission

@@ -0,0 +1,22 @@
+archive/EN_2021-10-14T23:27:47/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: 2022-10-01T14:30:44.231
+Launch V∞: [-1.5243188475966056, 5.9256671205622045, 0.2916154666540272] km/s
+Phase 1:
+	Planet: Neptune
+	V∞_in: [3.6975966998821526, -1.4215737222278524, 0.3088257373177974] km/s
+	V∞_out: [3.445686587806444, 0.6826200114085932, -1.001538192708208] km/s
+	time of flight: 2.855355071164953e8 seconds
+	arrival date: 2031-10-19T09:55:51.231
+	thrust profile: [-0.8759933715507354 0.9721696493713093 -0.019442309148699335; -0.8008537600952194 -0.5941302460728478 -0.06796587793610398; -0.627589785584642 -0.8318706537968823 -0.08563284635359299; -0.840841194502072 -0.9445735606822884 -0.0955284075050304; -0.3600239078894093 -0.47204355869564657 -0.11126127685731058; -0.7388484282650255 -0.7886435929888026 -0.08909986800032511; -0.32305894084141484 -0.30591569708824085 -0.10340952135470989; -0.28216239907675256 -0.1426792583554665 -0.1143226817898616; -0.09639141414540019 -0.011528842076150791 -0.26755240273453423; 0.18814683852103375 0.4893924983795105 -0.04759899728071763; 0.31623329829219116 0.48035347011008334 0.021140757522982417; 0.3495977355479997 0.48970181862122203 0.050702499356316995; 0.35078134471647493 0.5710967629548804 0.08085199199019613; 0.4242295692725758 0.6648754488413917 0.11708559827741634; 0.7544685450994223 0.6138555082590391 0.1547920784756316; 0.3078505072984024 0.6964463042108037 0.17903196782627837; -0.3363787766756175 0.3963963385214657 0.06482748384126795; -0.33655861967802553 0.3496684000706546 0.08953707892324089; -0.18529532214490396 0.27841610852846016 0.04136003156954945; -0.013754111231380713 0.1364854049755323 -0.023729392781819306] %
+
+Mass Used: 1572.0861495426557 kg
+Launch C3: 37.52211835324206 km²/s²
+||V∞_in||: 3.9734703394813478 km/s

archive/non_saturn/EU_2021-10-14T21:56:32.783/mission

@@ -0,0 +1,22 @@
+archive/EU_2021-10-14T21:56:32.783/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: 2022-06-06T12:32:32.955
+Launch V∞: [8.066701974215304, -5.184463452194054, 0.07048095785765573] km/s
+Phase 1:
+	Planet: Uranus
+	V∞_in: [0.41889683618179546, 1.9616780923678787, 0.0041185023421876354] km/s
+	V∞_out: [-1.0813442250676473, 1.269652537135473, -1.103843466471438] km/s
+	time of flight: 5.623145280158398e8 seconds
+	arrival date: 2040-03-31T19:01:20.955
+	thrust profile: [0.33113071235942554 0.37947009945825905 0.0026520116773191722; 0.14260319554091308 0.28557696226011836 0.004417291796288417; 0.06647276062018873 0.25607146683316817 0.0005698747089161628; 0.027229275899992078 0.22661317723264732 0.0037198450913083158; 0.005628941272053695 0.2174918155828432 0.0031209940137040507; -0.006857472637514542 0.18231095301617745 0.002901135182815245; -0.012538212235480179 0.17223842713204346 0.004083946247301381; -0.020554284983497238 0.14658209895894025 0.0024406319139407924; -0.0237765152614042 0.13969929590421654 0.0025319264516214923; -0.029588606341280674 0.12943480485169898 0.00277137925045028; -0.03356864687382611 0.1151446271614899 0.00248344129351035; -0.060200921677206726 0.09858718601646418 0.0030531971070393567; -0.059074407063264146 0.08879809946820336 0.003025672711349734; -0.07148477170551683 0.07027434840142367 0.002745785266915828; -0.084346554802205 0.048106266589968465 0.003300186254164532; -0.08365574756970999 0.04855533455534412 -0.004138826212145825; -0.06533683415745487 -0.0005908118552418543 -0.00015208190243403024; -0.1003833640846401 -0.032412953559420095 3.1819642175957066e-5; -0.08979147083557455 -0.0790505637439873 0.0014259188993576994; -0.0579299799142576 -0.14259393483414515 0.0009732733502837638] %
+
+Mass Used: 759.4776549013495 kg
+Launch C3: 91.9553095933655 km²/s²
+||V∞_in||: 2.0059093846683953 km/s

archive/non_saturn/EV_2021-10-14T13:05:26.925/mission

@@ -0,0 +1,22 @@
+archive/EV_2021-10-14T13:05:26.925/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 2000.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 1.0
+Launch Mass: 4000.0 kg
+Launch Date: 2021-10-18T09:45:17.709
+Launch V∞: [0.3617667798192156, -2.039064934241794, -0.4342053441028627] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [0.7379871188280966, -2.392854603152152, 1.8896396443096521] km/s
+	V∞_out: [1.5127292165463757, 1.3099790858071492, 1.5207956068242738] km/s
+	time of flight: 1.3532010222205028e7 seconds
+	arrival date: 2022-03-24T00:38:47.709
+	thrust profile: [0.11231015117371024 0.007222064740843916 0.047728104397320795; 0.12870381785557966 0.0566247978579788 0.21123650796860152; 0.12027023095334755 -0.008319633479200587 0.2578960766796108; 0.1347206943320554 -0.041609855302546406 0.30007660604057945; 0.19732275634506516 -0.048371534566925216 0.3566123678413536; 0.21018837696130593 -0.024190305368071867 0.38809649284784414; 0.28257952762883287 -0.010112243164057075 0.41959051839022865; 0.2845322594924626 0.05626043110186557 0.4427965235656657; 0.31989327360636083 0.10103389278981802 0.4572574662714401; 0.33347393333469577 0.06241718586254669 0.4778597182282868; 0.3395281862489285 0.10625631669191643 0.48095526186056015; 0.3383164423285961 0.1315535303664453 0.47222541173940435; 0.3311524095828194 0.16330336645453894 0.4609284090556696; 0.3201419295734179 0.1732833508978107 0.44244539961592666; 0.3013233347975498 0.20789558713014178 0.4227677382665769; 0.2721414750714771 0.17990409519215725 0.377125147146521; 0.198279076527229 0.21324470037966742 0.33028246998700145; 0.16370869214515785 0.10728022878269601 0.2608933387609283; 0.0684810317630511 0.08638181193636332 0.17016012690566112; 0.09669087307328576 0.06507874083792248 0.01466958168256049] %
+
+Mass Used: 183.95963971161564 kg
+Launch C3: 4.477195289882742 km²/s²
+||V∞_in||: 3.1370553270112 km/s

archive/non_saturn/EV_2021-10-14T13:07:15.278/mission

@@ -0,0 +1,22 @@
+archive/EV_2021-10-14T13:07:15.278/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 2000.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 1.0
+Launch Mass: 4000.0 kg
+Launch Date: 2021-10-22T22:17:17.936
+Launch V∞: [1.080421766777506, -2.0628288582618195, -0.4536456444832625] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [0.7677143929066254, -3.4082880069676302, 2.3505897429525078] km/s
+	V∞_out: [-1.2798972791822951, -1.4365988008982025, 1.4502645187385164] km/s
+	time of flight: 1.4034657251252254e7 seconds
+	arrival date: 2022-04-03T08:48:14.936
+	thrust profile: [0.1077661610742549 -0.09491507818452108 0.05312663076674047; 0.12462914010398723 -0.07372591873371813 0.073138215254182; 0.116881889714844 -0.06002677793428502 0.08095094342691629; 0.08293330133219345 -0.033724789600279505 0.12504790352006753; 0.09536827065302887 -0.004670650549755097 0.12635922504551902; 0.11091447261989335 0.004225864016796435 0.11537170625950409; 0.11303189248647355 0.03522866468488595 0.10914719877371856; 0.10740688646287562 0.06346630312429946 0.10249991019205282; 0.10449348372920764 0.05724537061115196 0.11359932836059951; 0.10049809726762707 0.07718474763324121 0.10349197510314542; 0.1007467313556788 0.08871232473224286 0.09586219439229779; 0.09639430875336537 0.10697634912585294 0.0790205018556672; 0.07665394337566692 0.1131155289012668 0.09223832705427028; 0.059511019561048636 0.12561664167233738 0.08431030720745564; 0.043597933388487026 0.13349728498081367 0.08121771907181134; 0.019379366866230683 0.14556439472332783 0.0634054361596215; 0.014456095940828476 0.14570335135746015 0.061398125952688364; -0.030752555428140677 0.1509195385631795 0.02876841287831368; -0.07387466238056084 0.13312162588233253 -0.034469925955284295; -0.02102718303541206 0.15219056670120726 -0.0065142822772471356] %
+
+Mass Used: 71.46119686087513 kg
+Launch C3: 5.6283684633630235 km²/s²
+||V∞_in||: 4.210829451211353 km/s

archive/non_saturn/EV_2021-10-14T13:09:46.191/mission

@@ -0,0 +1,22 @@
+archive/EV_2021-10-14T13:09:46.191/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 2000.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 1.0
+Launch Mass: 4000.0 kg
+Launch Date: 2022-08-27T18:20:28.271
+Launch V∞: [4.976680389443524, -1.705424182457512, -0.3485682941979716] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [4.210457531789055, 0.3638419019608806, 2.167260083943969] km/s
+	V∞_out: [-0.02718879860259023, 0.00013680384875937985, -0.40279343753838176] km/s
+	time of flight: 2.616182260016269e7 seconds
+	arrival date: 2023-06-26T13:30:50.271
+	thrust profile: [0.1081478833164793 -0.04747352000316829 0.009803784528203987; 0.11190267398595631 -0.08489441529847341 -0.007286984410559111; 0.12911430752493627 -0.11099328002003525 -0.01943723546946303; 0.16688603565301258 -0.12840027043968893 -0.02332008672269124; 0.21714048180407453 -0.1362382567528611 -0.02567076757100798; 0.2764401329174762 -0.13402041782174592 -0.0287511421326799; 0.33266188746520187 -0.11957670801586273 -0.031093308044346353; 0.3820659935956181 -0.09253553276581379 -0.031479580308358644; 0.41374954552181137 -0.05951601425001449 -0.03348539939450036; 0.4271557515022211 -0.02469794622072092 -0.03284633186694413; 0.4196852691041662 0.011180284532007942 -0.03287929676767141; 0.39104446127168524 0.05467052960463492 -0.03128098668740266; 0.3397344905954879 0.11008642002736206 -0.024504191585152588; 0.2681377457360699 0.17570003550101684 -0.016577172053069123; 0.046833731659678475 0.23938547094636797 0.008263855085563338; 0.20692889271962633 0.2635523571087766 0.020761614548693325; 0.13667494276947326 0.28012067330618706 0.033686527674503336; -0.11957290103408791 0.269968116350337 0.04482701107136116; -0.16727049842201927 0.21796253025589696 0.0361909665435463; -0.21921062997276963 0.1091389154173985 0.005030961855685549] %
+
+Mass Used: 250.70235015664184 kg
+Launch C3: 27.797319196502702 km²/s²
+||V∞_in||: 4.749457845699708 km/s

archive/non_saturn/EV_2021-10-14T13:09:51.898/mission

@@ -0,0 +1,22 @@
+archive/EV_2021-10-14T13:09:51.898/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 2000.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 1.0
+Launch Mass: 4000.0 kg
+Launch Date: 2021-10-18T18:36:15.124
+Launch V∞: [1.0916199935243702, -1.9934859843614063, -0.6362963816167255] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [0.5827260218152104, -3.245906754637226, 2.514356091647749] km/s
+	V∞_out: [0.7695910297576717, -0.7556093941856095, -0.9104795095643681] km/s
+	time of flight: 1.4088953343151927e7 seconds
+	arrival date: 2022-03-30T20:12:08.124
+	thrust profile: [0.03400397265810093 -0.1316395434244445 0.05699291900148288; 0.10473854742812332 -0.10525549757762309 -0.0006423273456525108; 0.11599902542775602 -0.06774249825652275 0.080606830950913; 0.1310987485805775 -0.04491628698617216 0.08120644367980684; 0.11533623131335603 -0.007730090103315951 0.12352673112630569; 0.11050163762503666 -0.014810624798424184 0.13358846300335825; 0.1368738413328123 0.031717507020523894 0.10537133013453537; 0.09607405762646531 0.039259635505570926 0.15075696692326396; 0.0932396587968502 0.050763423433988285 0.1524441259012387; 0.08835554978882662 0.06063431886658857 0.15285406762333867; 0.08337674859842645 0.07132142354385927 0.1521790088231852; 0.0783436520935084 0.07932345824922571 0.14956272424615258; 0.07190901949541267 0.09252700451278721 0.14364426645965755; 0.06152160664529564 0.10487327862985339 0.1337849292702545; 0.04522536761353614 0.12354914208182705 0.12221429106614988; 0.030730806933955798 0.1497661375884409 0.07201582662332497; 0.0013732827723847787 0.13783629400588643 0.09217277545311839; -0.047657124648179124 0.14299205548044944 0.04461491903740098; -0.04887637661869137 0.14261702502367085 -0.01118738193598132; -0.04624479767152048 0.12992926199532367 -0.060407791765814726] %
+
+Mass Used: 76.32181558799766 kg
+Launch C3: 5.570493665366048 km²/s²
+||V∞_in||: 4.146982858887446 km/s

archive/non_saturn/EV_2021-10-14T13:48:25.788/mission

@@ -0,0 +1,22 @@
+archive/EV_2021-10-14T13:48:25.788/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 2000.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.0005 kN
+	num_thrusters: 2
+	duty_cycle: 1.0
+Launch Mass: 4000.0 kg
+Launch Date: 2022-03-03T16:03:54.308
+Launch V∞: [3.1331875390553874, 4.743765316753105, -0.6321137349156039] km/s
+Phase 1:
+	Planet: Venus
+	V∞_in: [0.7336287799525429, 9.092380028023765, -2.060897868194347] km/s
+	V∞_out: [-0.005397228824250161, -6.841249447820443, 3.86835501811607e-7] km/s
+	time of flight: 1.431136134384693e7 seconds
+	arrival date: 2022-08-16T07:26:35.308
+	thrust profile: [-0.029700857947171155 0.037677806973394956 -0.0016513225652095235; -0.09203896237700117 0.06668008002755799 -0.003907365708797221; -0.15385799693549973 0.09456424369948617 -0.00567508250690443; -0.19644155536268554 0.12045167230584422 -0.010220562279956805; -0.28443665959408854 0.13387251178059187 -0.010826054663009434; -0.35314485464965406 0.1508209960737375 -0.014312066894957601; -0.42349740669156993 0.15073261096749926 -0.01617441359738227; -0.49179611760767494 0.1313289360663566 -0.019420534802667432; -0.5498265630622056 0.07689683044740066 -0.022535038089659315; -0.5841007485384517 -0.028343225924705343 -0.025645308771199683; -0.6463113947204338 -0.19361054238923944 -0.030545065432850942; -0.7020011201668798 -0.3987157016634757 -0.035892266940698137; -0.660261751730148 -0.564813684339657 -0.03928441369489666; -0.5533792180410886 -0.6697142859509423 -0.039751339872136054; -0.35878759946251465 -0.6287274757834188 -0.03432166295686523; -0.07897641529965045 -0.6890633639101433 -0.024417495241929963; 0.1132061820810732 -0.5814939033233674 -0.011948487492265437; 0.1525591439015402 -0.4915765280189982 -0.0025092936276034316; 0.10348417965356019 -0.4089525878329189 0.0030668463178562854; 0.024035973004629382 -0.3568182136414068 0.0051715969680988395] %
+
+Mass Used: 225.67816334678992 kg
+Launch C3: 32.719741309190596 km²/s²
+||V∞_in||: 9.351838631194836 km/s