Maybe nearing the final commit

archive/EM_3-29/EM_2022-03-29T21:26:22.750/mission

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+/home/connor/projects/thesis/archive/EM_2022-03-29T21:26:22.750/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-04-22T09:55:35.770
+Launch V∞: [7.3434961975052575, 2.1070520149056207, -1.014351173307538] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-4.0891408313442243e-10, -1.3519558171080589e-9, -2.9347938509608335e-9] km/s
+	V∞_out: [-1.009960237699357e-8, -1.009960237699357e-8, 7.767450588932219e-10] km/s
+	time of flight: 8.599031774086058e7 seconds
+	arrival date: 2027-01-12T16:07:32.770
+	thrust profile: [0.10180817450485931 0.010765994728988202 -0.007544294859875064; 0.16235850598372423 0.10642344368168269 -0.0003675622257710981; 0.1012089195326011 0.215498048785662 0.009263152266136488; -0.005263860097698059 0.23018146612119708 0.014653161556634695; -0.07216616837405394 0.1886632498893549 0.01482047592832661; -0.09398125027080778 0.12777759796739516 0.011338047777898999; -0.08181401680555038 0.06911303246065172 0.005833525852290107; -0.046580710304300145 0.02548722787737307 -0.000870777813142698; 0.0008108654501895264 -0.002069527547353827 -0.010201717802848145; 0.034561814232433444 -0.014025534635558886 -0.008973491598575703; 0.08747966934536043 -0.003895559625340753 -0.007112515261902957; 0.15550075175184433 0.018424169433452726 -0.005669922341139337; 0.20248982822207362 0.14526574995002947 0.0013158139705482853; 0.1119856201004996 0.257928321038749 0.011672620538172137; -0.013956968702964088 0.25905748898149866 0.016710191647944732; -0.08713823665180384 0.20616330494298554 0.01620667875500915; -0.10696574449396443 0.13889689572070454 0.012648766692620108; -0.09152920511480982 0.07897071043001104 0.008095327395193714; -0.05734765938030889 0.03602736492249166 0.004000200225081728; -0.018669314030212245 0.009667853783132363 0.0010959107001852323] %
+
+Mass Used: 102.10077631610102 kg
+Launch C3: 59.395512899082384 km²/s²
+||V∞_in||: 3.256994044580908e-9 km/s

archive/EM_3-29/EM_2022-03-29T21:29:32.797/mission

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+/home/connor/projects/thesis/archive/EM_2022-03-29T21:29:32.797/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-23T04:29:27.925
+Launch V∞: [3.3948803973755504, -2.4577679470301823, -0.9108626328289409] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-9.533352172826976e-10, -9.477177141496064e-10, -1.6329568148050564e-9] km/s
+	V∞_out: [-4.993330429282141e-10, -4.2879092581858787e-10, -2.3614363530159443e-10] km/s
+	time of flight: 1.7632014328727353e8 seconds
+	arrival date: 2029-12-23T22:18:30.925
+	thrust profile: [0.03456534559612611 0.003378817240313221 -0.005847373254693159; 0.00947257573188261 0.018201878458255185 0.007200303057438418; -0.004323909654354275 0.01249526284025378 0.0148773281730713; -0.01158118824683763 0.0035968703342061353 0.015269664673521784; -0.014059676447250516 -0.008412132946442719 0.008604541649422459; -0.005532635332091579 -0.0222637656012968 -0.0034383221186402285; 0.021986188048601012 -0.02106400050803527 -0.008639248086466517; 0.017681089333976076 0.009993783002874504 0.003021725433334957; 0.0019228014351383971 0.011070063719295309 0.013061259255238647; -0.006139542196052064 0.004677076522798168 0.015910259868307026; -0.008545089251963688 -0.004479324701411431 0.011537788412234507; -0.0016877898391656034 -0.011682836725100527 0.0011701415189322448; -0.0003566125916268421 -0.01179761558953741 -0.008519419526240076; 0.014749885872094748 -0.0029190252507672954 -0.0019352156873499635; 0.00424054036493813 0.005291076160963761 0.010144665911928733; -0.002562774524319081 0.0018319412240714573 0.0157273231044577; -0.004535441668234806 -0.00482430642022855 0.014079386327258895; 0.0021824954095405903 -0.011442073033427643 0.0056673371449387985; 0.00910349572655102 -0.00026356393299342343 -0.0060482701344148565; 0.0010618127127533534 0.0009141380026824337 -0.006122360667166782] %
+
+Mass Used: 24.97711287513448 kg
+Launch C3: 18.395506929817802 km²/s²
+||V∞_in||: 2.1150803439214027e-9 km/s

archive/EM_3-29/EM_2022-03-29T21:30:57.022/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:30:57.022/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-12T01:36:00.330
+Launch V∞: [-0.34441487078455013, 3.9103321083115397, 2.032019563693426] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-1.323280834421365e-9, -1.305249079827022e-9, -1.756498248174488e-9] km/s
+	V∞_out: [-2.072434338771005e-9, 3.1188692292717017e-10, -9.96060247089551e-10] km/s
+	time of flight: 1.9187428749374934e7 seconds
+	arrival date: 2025-05-22T03:26:28.330
+	thrust profile: [-0.0006647023892816537 0.004035322252316528 0.002450694309122812; -0.0010810936123367345 0.0033648421104130093 0.003041727879478422; -0.0013507121101609906 0.0028319436906776322 0.003294754033895274; -0.0013817337282281677 0.002283246633035519 0.003911472841560675; -0.0014099790469406482 0.0016622747910402052 0.004243346099566735; -0.0012603732201070137 0.0013617718291820912 0.004609732990326976; -0.001109687893062513 0.0010166792245012248 0.005257291391887101; -0.0009765487656423202 0.0007701050283466614 0.0045962916304727545; -0.0008511110507625 0.0005562454707099463 0.004264167411226241; -0.0007373982279473773 0.00044288704744547956 0.0042335052666390175; -0.0005724074417038922 0.0002590516109966243 0.003593127587839534; -0.00048097983471947337 0.00027784548514532824 0.0036573739539471012; -0.0004010082145124844 0.00023837273061184575 0.00295844216959782; -0.00030319886238157107 0.000188351968848797 0.0026590665546669954; -0.00013453010791864773 0.00015049323913512056 0.002533970064140107; -0.00017918516868998714 0.00011876509991415298 0.0020961759015662375; -0.0001309746244392474 9.400293297511669e-5 0.0016359370993405285; -8.735433670043718e-5 6.50059985134959e-5 0.0011999019334906667; -5.205594667799379e-5 3.959950287622984e-5 0.0007255745258836434; -1.69083877031164e-5 1.3250954732018612e-5 0.0002522304876801491] %
+
+Mass Used: 0.5263628244356369 kg
+Launch C3: 19.53842230774253 km²/s²
+||V∞_in||: 2.5573489052095017e-9 km/s

archive/EM_3-29/EM_2022-03-29T21:33:01.420/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:33:01.420/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-03-11T16:02:09.080
+Launch V∞: [7.290339628882368, -1.8288440801615886, -6.632030600228825] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.003664456556782759, -0.0036510052522354575, -0.0017682821659383713] km/s
+	V∞_out: [-0.1893444115511239, 0.18934441155112372, -0.07646642757306271] km/s
+	time of flight: 9.309960005487782e7 seconds
+	arrival date: 2026-02-21T05:02:09.080
+	thrust profile: [-0.1746457094907778 -0.05324520729862655 0.49134886061939687; -0.627027503294072 -0.40066969942751784 0.5818755748236487; -0.4247709197544459 -0.70455535681447 -0.18137441849457178; 0.39985450427415964 -0.6472758630327436 -0.6430237844213548; 0.4656645028614102 -0.26488366431804417 -0.7314105489598725; 0.1191067639913546 0.2223158565414293 -0.7468478853961351; -0.3933541564722199 0.058176480588614785 -0.7289724142316767; -0.5058338906252844 -0.4156231661282735 -0.5643546902998223; -0.5318185912755031 -0.6386622831457283 0.08080900296257724; 0.27321630774062744 -0.7220941798748955 -0.042143171437234374; 0.5425105272566577 -0.48807460643793443 -0.3531814327468772; 0.3522022888052473 0.06262879123129814 -0.6401364976996247; -0.1561236716305922 0.5164836976614604 -0.7196848157274702; -0.6067507933991897 0.5079757344850814 -0.7392991893046754; -0.7130116758304386 0.10035106755129632 -0.6845824948634448; -0.6878836289874771 -0.5954631055945753 -0.6809457412241607; -0.3269757395259158 -0.7281706083760071 -0.725121591528696; 0.5029082823724691 -0.7211592525685994 -0.6308100968795103; 0.5368458661526178 -0.4216537659711369 -0.14188422812553816; 0.16194407043490938 -0.2071575272584137 0.018329982767622783] %
+
+Mass Used: 633.2884274220719 kg
+Launch C3: 100.4775524563663 km²/s²
+||V∞_in||: 0.005466708610011581 km/s

archive/EM_3-29/EM_2022-03-29T21:44:52.679/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:44:52.679/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-01-22T12:08:19.865
+Launch V∞: [9.999999510580688, -9.997198712980596, 0.2367016801977378] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.000819918545143649, -0.0012451509155042646, -0.001250921976389137] km/s
+	V∞_out: [0.0019338785602035886, -0.0019338785602035886, -0.0006601321083539838] km/s
+	time of flight: 1.7233962915051136e7 seconds
+	arrival date: 2024-08-08T23:21:01.865
+	thrust profile: [-2.3909756762714905e-7 3.7137254328500285e-7 6.84557970113123e-10; -6.490849187612506e-7 -1.6923622503113822e-7 7.597297006308147e-8; -1.3462011970258392e-7 5.4785730096847575e-8 3.065595287593101e-8; 0.15976947743667638 -0.2920794439050224 0.002394761620150665; 0.5616910709675398 -0.7901992734350411 0.010726222487855458; 1.0 -1.0 -0.0032456678933753843; 1.0 -0.6953371235997132 -0.00807847832727659; 1.0 -0.23068593990468247 -0.009476805297354552; 1.0 0.06616898317798338 -0.009396139547492788; 0.8458292750604345 0.20752997653151717 -0.009416373557718996; 0.4899942520164369 0.18998472141046954 -0.007666776709170746; 0.03957676169176063 0.0210088124260986 -0.0012531497610165998; -5.452577185178014e-7 -3.4799035186607614e-7 -1.0511021967736704e-7; -1.3251613739747719e-8 3.0514099445579054e-7 4.002333800730656e-8; 1.6516923938790852e-8 -9.029916507496571e-8 8.144270988392475e-8; 6.025616118742147e-7 -5.477234118696148e-7 1.5445834673209101e-6; 1.2522336398625811e-7 -1.1634639614565971e-6 3.2890058545783734e-7; -1.8707392087284995e-7 1.037143716480063e-7 2.3487962795435016e-7; -1.0032847526436222e-6 -9.961208338104671e-7 1.0945507651240803e-6; 1.5694593639258316e-6 -4.2952948369892885e-7 -3.8494467904625947e-7] %
+
+Mass Used: 50.813640071233294 kg
+Launch C3: 200.0000000038433 km²/s²
+||V∞_in||: 0.0019461431124315834 km/s

archive/EM_3-29/EM_2022-03-29T21:46:54.102/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:46:54.102/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-11-11T17:47:11.536
+Launch V∞: [-2.637789291564701, 7.365806125093766, 1.1946168639279173] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.044388255339722446, 0.05279424355864281, 0.05040248633053719] km/s
+	V∞_out: [-0.014690038570962082, 6.047928149069252, 0.0402218040709599] km/s
+	time of flight: 9.338400004077721e6 seconds
+	arrival date: 2025-02-27T19:47:11.536
+	thrust profile: [4.550817449124052e-7 7.763476095695704e-6 -8.951834889878114e-5; -1.683989066220231e-5 6.926242475714976e-5 -2.8801022778955843e-6; -3.2857446755970286e-5 0.000111131319945128 5.116462056209784e-6; -1.8729031546388233e-5 5.436146435025702e-5 8.422047807261321e-5; -3.937488649940267e-5 0.00012696227955243206 -8.532134224201484e-5; -1.0059863865866885e-5 2.4658136117281536e-5 -1.684375841787375e-5; 4.906742377377519e-5 -0.00012829316592757872 0.00011336735200215563; 2.089328062485444e-5 -4.091796173674061e-5 4.91054297730873e-5; 3.6303103564460345e-6 -8.192507389662463e-6 0.00018463100624064758; 9.183017844786658e-5 -0.000102961513685098 -2.2996942742832565e-5; -3.570454906404795e-6 7.063475253086773e-7 4.489457323974194e-5; 4.501722144285221e-6 -1.4070298502410475e-5 0.00012324041685903012; -1.7478055220611036e-6 2.873220524346435e-5 -0.0002474631986841141; -2.3178341505326345e-7 6.162662443854e-5 -0.00036775871159988626; 5.113474717292926e-6 0.00011622972164925676 -6.003368153265286e-5; 3.496467618704115e-6 2.008310733865503e-6 -3.261195379666672e-5; 7.630237920042993e-6 1.1841800841292385e-5 -5.3531357169394734e-5; -2.435474741947106e-5 -3.088566762921298e-5 8.568030368819686e-5; 2.05686426229734e-5 2.1197875883934535e-5 -3.1608864977248355e-5; 2.6389349541919505e-5 2.927984365861755e-5 9.508078462673436e-6] %
+
+Mass Used: 0.00865322013714831 kg
+Launch C3: 62.64014167074321 km²/s²
+||V∞_in||: 0.08542809838298922 km/s

archive/EM_3-29/EM_2022-03-29T21:49:25.266/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:25.266/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-01-22T05:21:14.524
+Launch V∞: [9.999636707630842, -9.999711031426283, 0.11421476860707167] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.0005668718069816592, -0.00031760816291536434, -0.000716139266867567] km/s
+	V∞_out: [4.602661802552677e-5, -0.0002767853386654524, -0.0009253970079822862] km/s
+	time of flight: 1.8504181207751602e7 seconds
+	arrival date: 2024-08-23T09:24:15.524
+	thrust profile: [7.857635262435799e-9 -1.3269126706634187e-9 -2.6678444933858832e-8; -1.0637360281620793e-8 -2.286988515481341e-8 -8.80823866575928e-9; 6.0952069265027294e-9 -2.83469800266583e-8 -1.490175153809855e-8; 0.0226345802482894 -0.0425037954420528 0.00013571022638739796; 0.3150512263564853 -0.3307029057599246 6.642556817831003e-5; 0.7436637294478844 -0.4801347645399363 -0.0017893772307274593; 0.8606779112586623 -0.24141142990090325 -0.0037932113948367296; 0.8040060250257044 0.016198399857395514 -0.004471603451557433; 0.6399746211803117 0.16197029278741412 -0.0044542497883041455; 0.3727551022451268 0.16851762370795223 -0.0032249765404340643; 2.1347115495508663e-7 1.2358201767787164e-7 -9.95030121314948e-9; -3.2446413607840104e-9 -4.6723722793820385e-9 -1.7929106379494995e-8; 5.182519495541647e-9 3.4030707061963687e-9 1.3576577417457207e-9; 7.77921539082814e-9 8.910703811213887e-9 -2.795024270457183e-9; -6.239445899255738e-9 -5.3493145318475e-9 -1.0884699785346293e-8; -4.6105410818633964e-8 1.0422534641378147e-8 -3.1989587412074714e-8; -5.043811123979896e-10 -1.5735249773983739e-9 -2.485221976312311e-9; -2.9761057764991258e-9 5.873921191568738e-9 -9.103537944568155e-9; 5.14444314540825e-9 2.6244355859150998e-8 -4.4579652417185817e-8; 1.7864549904100225e-9 -5.672782066774026e-9 -8.346804698233242e-9] %
+
+Mass Used: 30.632832509893888 kg
+Launch C3: 200.00000000999466 km²/s²
+||V∞_in||: 0.0009669922648350091 km/s

archive/EM_3-29/EM_2022-03-29T21:49:36.826/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:36.826/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-15T10:56:11.057
+Launch V∞: [6.441902798268679, 10.0, -0.8580312930039031] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [1.1346777920325148e-7, -1.6337616718675993e-7, 1.0330204534180961e-7] km/s
+	V∞_out: [-1.0317733873112507e-7, 2.3171717331048837e-6, -1.93986714938645e-8] km/s
+	time of flight: 3.4632733537038654e7 seconds
+	arrival date: 2025-06-20T07:08:24.057
+	thrust profile: [-1.6714820918342543e-8 -1.528466539382287e-8 -2.1954025843586096e-8; -3.349740604524035e-8 1.7981805687302658e-7 -7.022649953046174e-9; 1.8833170950448843e-8 8.548553623260635e-8 -4.108646810746605e-9; 0.015250670354150446 0.8084120898285189 0.022810952919723303; -0.4471453131878308 0.9999999903024106 0.04006905981158459; -0.940578331193299 0.999999993466643 0.0463151648707486; -0.9999999926560775 0.8872505298154237 0.043065678915645736; -0.9999999865564515 0.5078822642356666 0.04002774379588722; -0.962703858267274 0.25286276492713566 0.031382869157176016; -0.7756546264427393 0.08215017131953659 0.018158411737504068; -0.5391748150704597 -0.00685832535402532 0.010123577086814562; -0.28342464446445065 -0.029810747488727737 0.006770186169348639; -1.123224049355356e-8 -1.3141710495594749e-8 -1.7542653699628666e-8; -1.7528478886241226e-7 5.358445351823748e-9 -6.699375227774894e-8; -1.3135303081170559e-7 -1.2185271425829965e-7 -3.228097411495359e-10; 1.1373627184214759e-8 3.001014188079098e-8 -2.51036875849398e-8; 3.6364423359808617e-12 -1.1453961586869118e-7 3.15681037477465e-8; -2.2731576792249495e-8 -7.140875056921905e-9 -4.234566273922648e-9; -8.105071719032486e-8 -1.2311649733884225e-7 5.2532523546505e-9; 3.7930997639741155e-9 2.2050999807275034e-9 -1.6994076482759186e-8] %
+
+Mass Used: 114.99761554896395 kg
+Launch C3: 142.2343293621158 km²/s²
+||V∞_in||: 2.2413839807974726e-7 km/s

archive/EM_3-29/EM_2022-03-29T21:49:40.929/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:49:40.929/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-14T20:37:13.182
+Launch V∞: [-1.1330208167169828, 8.150093305408548, -0.42599383797196094] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [0.06785386315763219, 0.08160526029107552, 0.10069188976102801] km/s
+	V∞_out: [-0.06019693846168101, 0.1154681190090172, 0.0013638641321443625] km/s
+	time of flight: 3.3249599821579646e7 seconds
+	arrival date: 2025-08-03T16:37:12.182
+	thrust profile: [-3.2390308133578046e-6 -8.205592041810102e-7 -1.7023725789005115e-6; -4.254648394564359e-6 -1.0681074705420982e-5 7.03349069144519e-6; -3.6503599525277004e-5 1.211591857880556e-5 4.998821545861222e-5; 5.8142912412027884e-6 1.815497639490963e-5 4.755326622471413e-6; 2.1131283188873194e-5 -2.658343343429692e-5 -1.3407885571598285e-5; -4.61924068664863e-6 1.233572876146752e-5 5.931451952243551e-6; -1.0093023108865622e-6 -6.117529097643235e-6 -1.4487022912767236e-5; 3.255742051919883e-5 2.414843899996706e-6 -1.6802467693339598e-6; -3.755099218079546e-7 -7.03737787215465e-6 3.678113986874362e-7; 5.000413950443672e-6 -6.750857750004181e-6 -3.69195982831641e-6; -4.843006060165484e-6 -3.981873834068709e-6 -8.39506817046051e-6; 1.9138464837736528e-5 -1.1967250409666853e-5 -5.84236755572486e-5; 1.9835599971523244e-5 -7.450220189850961e-6 -3.2160727631147586e-6; 5.835552646320366e-6 -1.8859087544603728e-5 -9.49615711370029e-6; -2.455723410768635e-5 6.327003737755019e-6 -1.2577725131349784e-5; -5.262439904045446e-6 6.952002003737397e-6 -6.5460093506210335e-6; 1.29796109554274e-5 1.82478532330856e-5 -1.5041887536003234e-5; -9.627406878153045e-6 -5.772049645592626e-6 -1.4348219890042947e-7; -9.78894081123465e-6 3.3042544258109555e-5 1.5879718352840226e-5; -5.425039696689593e-7 -9.226404572856256e-6 9.61839430152342e-6] %
+
+Mass Used: 0.006099916057792143 kg
+Launch C3: 67.88922780796933 km²/s²
+||V∞_in||: 0.14629566608835642 km/s

archive/EM_3-29/EM_2022-03-29T21:51:28.498/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:51:28.498/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-29T06:36:19.325
+Launch V∞: [-2.587284640962116, 4.633341500696843, 1.7167586419161047] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.19753746109783032, 0.25819074680887755, 0.26503536879040035] km/s
+	V∞_out: [-0.315758776271297, -0.8539914904213332, 0.8539914904213984] km/s
+	time of flight: 1.5073200002586758e7 seconds
+	arrival date: 2025-03-22T17:36:19.325
+	thrust profile: [-7.450599065824146e-9 -7.450584303466995e-9 -7.450590836663176e-9; -7.450587576906885e-9 -7.450589090923008e-9 -7.450558189003243e-9; -7.450565194803655e-9 -7.450611457729077e-9 -7.45054991590754e-9; -7.450600513649451e-9 -7.450590716301945e-9 -7.450607153363093e-9; -7.450528020006835e-9 -7.450561990165038e-9 -7.450526461597745e-9; -7.450555250204573e-9 -7.450607011409635e-9 -7.450602548674602e-9; -7.450564628439462e-9 -7.450600629100434e-9 -7.450588565463268e-9; -7.450619650423247e-9 -7.450608473513382e-9 -7.4505692480758075e-9; -7.45064263594121e-9 -7.450567115419777e-9 -7.450562075663264e-9; -7.450580126235538e-9 -7.450587476295809e-9 -7.450568854754488e-9; -7.4505366612824064e-9 -7.450589324902333e-9 -7.450584239263405e-9; -7.450489666957581e-9 -7.450537925286817e-9 -7.450498460628677e-9; -7.450552685353022e-9 -7.450579447503591e-9 -7.450633939663657e-9; -7.450616725224094e-9 -7.45060730810255e-9 -7.450610502067296e-9; -7.450581072447471e-9 -7.4505612150820725e-9 -7.450606871304834e-9; -7.450563685058705e-9 -7.450550577646896e-9 -7.450584512906325e-9; -7.45058338424796e-9 -7.45058208960814e-9 -7.45059162827976e-9; -7.450547249176265e-9 -7.450555252809561e-9 -7.450551428356576e-9; -7.45060469168066e-9 -7.450619817820747e-9 -7.450626574693086e-9; -7.450591348730228e-9 -7.450569077582649e-9 -7.4505992975666e-9] %
+
+Mass Used: 1.549092758068582e-6 kg
+Launch C3: 31.109155510031766 km²/s²
+||V∞_in||: 0.4194368331281437 km/s

archive/EM_3-29/EM_2022-03-29T21:58:30.321/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:58:30.321/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: 2024-12-10T18:17:03.345
+Launch V∞: [-0.22142913746497983, 8.613702367564114, 0.395646369589788] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.003807700964755288, -0.05635954129158412, -0.008059749565666045] km/s
+	V∞_out: [-0.004673762071972183, 0.023969198600263253, 0.0032827185153388007] km/s
+	time of flight: 2.211840042633046e7 seconds
+	arrival date: 2025-08-23T18:17:03.345
+	thrust profile: [-2.7099961488351806e-5 -1.4871074056565297e-5 -2.4409683044127975e-5; 9.646611740529691e-6 -0.0003420396277143331 -1.4868108643254946e-5; 2.133935422770787e-5 -4.4306217453697985e-6 -4.803508959276009e-5; 2.4459845792704493e-5 -3.6995123289765117e-5 -2.9925040076576046e-5; -3.650950167903471e-6 -7.838803352580581e-5 2.4747499455879648e-5; -6.523041671648795e-5 3.5087934323253556e-6 -2.4005599476677803e-5; 2.5824401386028627e-5 -5.305113471826212e-5 4.630647640937965e-5; 3.106981203665597e-5 3.544948660180863e-5 5.523446183421823e-5; 5.22286273436312e-5 0.000123040814806458 -0.00012676926781162037; -7.230267382777404e-5 -0.000260285686999283 0.00028378411056846934; -6.687818964937921e-5 0.00010386642943476749 -1.7433504223833023e-5; 1.628396440937132e-5 9.706470918419143e-6 -2.010464752776144e-5; 1.7691694085809603e-5 1.8769928239818888e-5 8.64374415484856e-5; -1.9940109128613944e-5 -2.4978683584950083e-5 8.154400491960929e-5; 3.746496390446149e-5 -7.996841154215747e-5 8.731190252691787e-5; 8.384626723016047e-5 0.00012055180341030887 -9.12903721447452e-5; 0.00030557244279303915 -1.0874417231438263e-5 0.00027076266521899666; 0.00010797337086871226 2.418131034629288e-6 2.46314050788356e-7; -4.8544246038547224e-5 8.023388406493804e-6 -1.3321622294600293e-6; -2.1337222473883922e-5 0.000161247930621023 -9.715049457277587e-5] %
+
+Mass Used: 0.024185192960430868 kg
+Launch C3: 74.4014353896677 km²/s²
+||V∞_in||: 0.05706010904560232 km/s

archive/EM_3-29/EM_2022-03-29T21:59:56.201/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T21:59:56.201/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-11-02T06:44:24.402
+Launch V∞: [-0.049611423370383025, 4.3887768099156235, 0.2397844149782377] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.28117135821620853, 1.194065776563358, -0.1878338484580809] km/s
+	V∞_out: [-0.6401552299219904, 1.0676650444881157, -0.004843562733730455] km/s
+	time of flight: 2.8675341966952853e7 seconds
+	arrival date: 2025-09-30T04:06:45.402
+	thrust profile: [-6.75010685435156e-9 -7.128389367903114e-9 -6.764569952771536e-9; -7.854492591597582e-9 -7.999190980986096e-9 -7.56171297045386e-9; -7.411321266505082e-9 -7.3114050701082215e-9 -7.55580573230112e-9; -7.651530680516069e-9 -7.666997827122132e-9 -8.49436628413585e-9; -8.211778239957757e-9 -7.712874354717269e-9 -7.531646409796486e-9; -1.3041223632506712e-8 -1.1505347567528765e-8 -1.1327175955299429e-8; -7.4382917597938215e-9 -7.470595276285478e-9 -7.436526503122886e-9; -7.4066384907957325e-9 -7.477391356913722e-9 -7.393627041672364e-9; -8.490728461637439e-9 -7.447948593375514e-9 -8.223435454942976e-9; -7.243567265436005e-9 -6.990848569720015e-9 -7.311069521989123e-9; -7.470925069700345e-9 -7.517096742281904e-9 -7.2858921115831336e-9; -5.251447999281985e-9 -5.273780973491265e-9 -6.675361320542912e-9; -7.558627194101523e-9 -7.492146820031137e-9 -7.45645012297696e-9; -7.2878343544302096e-9 -7.2766617254979426e-9 -7.221830929334092e-9; -1.5590145011707196e-9 -1.974892338935215e-9 -1.3189839304906718e-9; -4.649692239474741e-9 -5.02145900568508e-9 -3.3671118225301505e-9; -7.850732664606476e-9 -7.768068826428585e-9 -7.4479836858425065e-9; -7.24166072771011e-9 -7.280881665927263e-9 -7.234374477741455e-9; -5.484578641350827e-9 -5.45192526011684e-9 -5.410771310297238e-9; -7.621367481763838e-9 -7.564226463702764e-9 -7.592122009986836e-9] %
+
+Mass Used: 2.8080553420295473e-6 kg
+Launch C3: 19.321319746248445 km²/s²
+||V∞_in||: 1.2410205341039189 km/s

archive/EM_3-29/EM_2022-03-29T22:02:40.626/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:02:40.626/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: 2024-12-05T12:41:35.605
+Launch V∞: [0.34208345982054794, 9.685722102267114, 1.0135726196799333] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-1.044189695816697, 5.606992695460721, 0.6669749140025341] km/s
+	V∞_out: [-1.663147851968031, 4.139628155579746, 0.7399548282520139] km/s
+	time of flight: 1.1581200001669213e7 seconds
+	arrival date: 2025-04-18T13:41:35.605
+	thrust profile: [-4.6079105664078877e-5 -0.00012331290696458524 3.857290588633784e-5; 1.080629253868903e-5 -7.862558725402423e-5 -1.577782579822753e-5; 0.00012294508889228685 0.0001157766111977547 -7.561217621375722e-5; 7.982229075851814e-5 -3.220285538923316e-5 -4.4317366310939693e-5; -2.379024823156827e-5 -7.848301760916924e-5 1.0173976438826385e-5; -5.0258317369872474e-5 -9.493318759847104e-5 2.0214040124684093e-5; -5.091418646156128e-5 -0.0001217205174737956 1.2898657418352046e-5; 2.8918514216456975e-6 4.8713183689657356e-5 8.218982364067898e-7; -7.013970277251351e-5 0.00016984599894599242 4.472426555147454e-5; 4.101982487628375e-5 -0.00014567448690259096 -4.20309304000344e-5; -4.70029927248979e-5 -8.284004507475568e-5 1.8925597178656232e-5; 8.670365778542101e-5 7.723828389414057e-5 -4.728960557142774e-5; -1.1273042710496325e-5 1.5796318007177794e-6 1.004719027628209e-5; 1.156788959809497e-5 -9.12107530024284e-5 -4.421958910455016e-5; 5.8489607768559684e-5 -3.186318691478282e-5 -7.568690979128904e-5; -4.101390839132036e-5 -6.912092662580811e-5 1.875683893727222e-5; -9.282793252271017e-5 1.8581365311066747e-5 0.0001607242504965489; 2.5608653889505896e-5 2.5749263651290097e-5 -2.663654795135107e-5; 6.471735913709624e-6 -1.582848279061017e-5 -3.144105357929748e-5; -2.0418356210322056e-5 -5.206011476136069e-5 1.0750219832116774e-6] %
+
+Mass Used: 0.009526397249373986 kg
+Launch C3: 94.95756319119332 km²/s²
+||V∞_in||: 5.742260421097979 km/s

archive/EM_3-29/EM_2022-03-29T22:11:59.808/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:11:59.808/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-07-12T14:57:14.038
+Launch V∞: [-2.1356055281697612, 10.0, -9.769298185542464] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-1.4198898735875047, 1.3740951409636546, -1.4192321863480188] km/s
+	V∞_out: [1.4110404995307853, -2.1212048062899553, -0.6728408923695377] km/s
+	time of flight: 1.5440221824979678e7 seconds
+	arrival date: 2025-01-07T07:54:15.038
+	thrust profile: [0.05956977091681903 1.0 -0.10922677780373319; 0.23817833345981507 1.0 0.09826946570814477; 0.40293966085543176 1.0 0.3551237041998419; 0.5317072540959735 1.0 0.7307023601163831; 0.5078043727484851 1.0 0.9982992529843099; 0.33655425425041224 1.0 1.0; 0.1360349738666649 1.0 1.0; -0.026672364591518467 1.0 1.0; -0.19610649486002443 1.0 1.0; -0.29528444695253986 1.0 1.0; -0.35123463549962813 1.0 1.0; -0.3634631832054668 1.0 1.0; -0.34243556937322644 1.0 1.0; -0.2988969593988343 1.0 1.0; -0.23211645533604322 0.8701239790258618 1.0; -0.13699199073043578 0.48199643592034935 0.6802560133378645; -4.9400538315483375e-8 1.4543622135653008e-7 2.2274035599587473e-7; -2.6590282235167093e-8 6.069199505306199e-8 7.406086114073912e-8; 7.262188061710368e-8 -2.6660015831706114e-8 -1.054025466018286e-8; 7.299781920337516e-9 5.276251956583804e-9 -2.5519508317922344e-8] %
+
+Mass Used: 130.30806476829775 kg
+Launch C3: 199.99999800999254 km²/s²
+||V∞_in||: 2.432785380649605 km/s

archive/EM_3-29/EM_2022-03-29T22:26:29.640/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:26:29.640/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-05-10T14:47:37.584
+Launch V∞: [8.454590640928295, 9.260765024912534, -0.9885318724952183] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.006319696103929528, -0.0412349395695302, 0.025407019305862494] km/s
+	V∞_out: [0.022415695471427622, -0.032554221329412304, 0.028687979305271248] km/s
+	time of flight: 1.8230010689416587e7 seconds
+	arrival date: 2024-12-07T14:41:07.584
+	thrust profile: [-0.0002622529733463554 0.00010449975350988813 -0.00012030102951252053; 2.2564340820408038e-5 -3.981832926552484e-5 -7.923191359546866e-6; 5.169422416636556e-5 -5.810036687510864e-5 0.00011428268526115506; -0.00014971921355914664 -0.00014100200005065646 0.00016890254129742059; 0.00015620328410727985 -3.366292385390309e-5 -0.00020340087014733029; -3.210609078978168e-5 -6.498562052193143e-5 5.338807325839352e-5; -8.516237377437068e-5 -0.0001612296252470605 4.209812632127493e-6; 6.305171484191589e-5 -0.001682367723787057 3.8599641512170114e-5; 2.2345674659450702e-5 6.798172919803859e-5 -0.0001184406426706027; -1.6251278244512348e-5 -6.533351590187232e-5 -3.92438433311786e-6; -0.00036512149400096404 -4.6068321314717516e-5 -5.609213629078427e-5; -5.621377289755845e-5 2.1241246976381148e-5 -3.414115489177037e-5; -0.00034119461694600184 -6.972852980194507e-5 2.2003699273903694e-5; 0.00018976563510694219 -9.050300294247073e-6 0.00012300348192681063; 5.426150865573059e-5 -0.00010044444909460297 4.785290273646994e-5; -4.4309429079208605e-5 7.02628779669344e-5 -4.7916743218706474e-5; -8.408538773370183e-5 -4.412949196949812e-5 2.4492265814848663e-5; 0.00011172380033234707 6.642438716286984e-5 9.399896039444412e-6; 8.401331768830077e-6 4.877367093015932e-6 -1.2408399381198787e-6; 9.503407085636648e-5 -0.0002551562074474474 -1.3659784774574114e-5] %
+
+Mass Used: 0.03575572314321107 kg
+Launch C3: 158.21906701525444 km²/s²
+||V∞_in||: 0.0488444001924202 km/s

archive/EM_3-29/EM_2022-03-29T22:29:19.608/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:29:19.608/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-10T01:24:19.159
+Launch V∞: [-1.361280774218496, 4.248905515475195, 1.6131303371846983] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-1.3206429765527528, 0.04508054081073763, -0.10860236471971149] km/s
+	V∞_out: [1.3258015388055073, 0.008890670618699885, -0.015202352520394155] km/s
+	time of flight: 1.6044052824580787e7 seconds
+	arrival date: 2025-04-13T18:05:11.159
+	thrust profile: [-9.649476733530478e-5 -3.874129604104022e-5 0.0001243676257598534; 0.00017944991783773494 -0.0003021068710903314 -0.00023906829442885233; -1.2520197657221369e-5 7.529839362963302e-5 5.22491643077963e-5; 6.0473365960938625e-5 -0.00010443015036179195 0.00013074051319186437; 0.0006044516898117107 -0.00017952114259198458 7.975422345770218e-5; -1.5105320951034641e-5 5.488422632601538e-5 -3.480125630187902e-5; -0.00035693490512667196 -2.9324170471654634e-5 9.386409045588269e-5; 0.0006536233376695634 -0.000323215551438777 -0.000991075858075292; -0.00048048705998534366 -0.0008846136053753608 7.485312552148982e-5; 0.0002457539906734169 2.3610783147200267e-5 0.00031354855012369744; 0.0003084291416236774 0.00030133549870160124 0.00012216085485925468; -3.145870054396133e-5 9.600064248608948e-5 -0.00017139285888021958; 0.0002323428803906647 -0.0003932431132474737 -0.00038269549666544874; -9.648756923300717e-5 7.371414257236465e-5 -0.00010492608262327025; -0.00016513882219009883 5.681301427250039e-5 -0.00023413816734468073; 0.0001688227002363334 3.9296604381294236e-5 -0.0002465079878323193; 4.223349001330004e-5 0.00018462477409466818 0.0004274596352430292; -7.266996009870076e-6 -0.00023420474628868667 3.054421622059266e-5; 4.4599716714522025e-5 -0.00015080232626015259 -0.00017624139057002226; 2.058233894174994e-5 -2.9681895453803056e-5 0.00010285445493880417] %
+
+Mass Used: 0.04864906937473279 kg
+Launch C3: 22.508472910438055 km²/s²
+||V∞_in||: 1.3258674897215847 km/s

archive/EM_3-29/EM_2022-03-29T22:35:03.801/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:35:03.801/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-15T00:59:25.735
+Launch V∞: [0.08411754828864794, 3.867780292357817, 2.507975455218117] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.01111567461793714, -0.2019526290080634, -0.10099494494608693] km/s
+	V∞_out: [0.05863131293194478, -0.1437072200747788, -0.16341819092150492] km/s
+	time of flight: 2.122969403809613e7 seconds
+	arrival date: 2025-06-17T18:07:39.735
+	thrust profile: [-0.0019253353195135495 -0.006208595765491277 -0.0030413706831210283; -0.005094954059343889 -0.006884862652799308 -0.007716049803660748; -0.001169679362784149 -0.003040509785898553 -0.0023827736029818115; -0.0009800602675577555 -0.005005973318342694 -0.0007235675342944551; -0.0035541375195941027 -0.0010759580832810519 -0.0011368932928665326; -0.004023727803229634 -0.0024144419030426778 -0.0020601786180336804; -0.009415901341030907 -0.007648304620004416 0.008910953721132594; 0.00019160911662570728 -0.00041311185476429913 0.002747155966524439; -0.0005053512629044138 -0.000435305465528584 0.0010810134121178056; 0.0018400336528207576 -0.006748721129952468 0.002259933413232509; 0.00022745932395296879 0.010666778341568943 0.0035537786550811704; -0.0004423321131218159 -4.1278833244748e-6 0.0012966352168264361; 0.00584099379819922 0.010506361039734275 0.0023162665551785394; -0.0013489272396317838 -0.0016553055603146898 0.00247736021958195; -0.0003060718810677023 0.0030689000185227426 -0.00026453391075189313; -0.004902002300222478 -0.006091743775746333 -0.0007723370782334376; -0.0010727586684161662 -0.0015117821322166705 -0.0011100152254532457; 0.001981284413785558 0.002082711629710382 0.000757647029883398; 0.0002652136199514425 -0.004511943969868106 0.0007431379304516129; 0.0007883244474613861 -0.00476964812130089 3.034140598992801e-5] %
+
+Mass Used: 0.9889560483511559 kg
+Launch C3: 21.256741035858134 km²/s²
+||V∞_in||: 0.22607167334751047 km/s

archive/EM_3-29/EM_2022-03-29T22:38:25.802/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:38:25.802/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-10-07T17:37:26.448
+Launch V∞: [-1.132800064227913, 4.057296625668816, 1.8160423657393692] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.09025126720242063, -0.16294649165165395, 0.002018029101130675] km/s
+	V∞_out: [-0.18204756492089805, -0.026081869886201665, -0.0286582298370937] km/s
+	time of flight: 1.7138821243684784e7 seconds
+	arrival date: 2025-04-24T02:24:27.448
+	thrust profile: [-0.001053336200227854 -0.00028654474915887655 -0.0003820424031938627; 0.0008512529608243817 0.0008846317646016004 0.00025282033285603365; 0.00042096876484458586 -0.000407673670480482 -0.000928628092675361; -7.585307650884643e-5 -0.00013518461742213344 0.00156643510514752; 0.0008460627785635593 -0.0007843263217494761 -0.0007202803479853547; 0.002018749793184083 -0.00017983404176264242 -0.0006659097248956292; 0.00040668294946816447 0.0009420606711834561 -0.0007751842339076142; -0.0002948940003770048 1.1828072211327191e-5 -0.00013445879115795128; -0.0004411373325257146 0.002302823369497903 0.0007032460495624283; -0.0004305359949988352 0.0003086368359122586 -0.00012577020060691192; -0.0004796057040344445 0.00048325375373444216 -0.0012858708318398222; 0.0007082846291908338 0.0014131843493881463 0.0012334716036545182; 0.0007516628476279127 0.00019283672154011742 -0.00047698959544296255; 2.8585166048847224e-5 0.0004721397839283915 -0.0004494052618972365; 3.140121868826565e-5 1.8672409758238784e-5 -0.0010892419657405827; -0.0012387600934636242 0.0010224726118372646 0.0005096784526400515; 0.0004830392791164112 -0.00018504611294579005 -0.0007919144470676173; -0.0002823515956750592 0.00015118295801919124 -0.0004211043216927825; 0.000699667738192727 0.0008572250810665738 -0.00044787467026235686; -0.0013106710074165672 1.8187501171149852e-6 -0.0013087579926788614] %
+
+Mass Used: 0.17400800233144764 kg
+Launch C3: 21.04290176833857 km²/s²
+||V∞_in||: 0.18628183704988058 km/s

archive/EM_3-29/EM_2022-03-29T22:49:56.957/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:49:56.957/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2024-09-12T20:18:50.704
+Launch V∞: [-1.2901325972737976, 3.5232401246782135, -4.555427856822656] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-0.47357409467459016, 0.6120735570744102, 0.2493748383223478] km/s
+	V∞_out: [-0.5474046060397546, 0.593375716049692, -0.4503838007744617] km/s
+	time of flight: 2.33568000005211e7 seconds
+	arrival date: 2025-06-10T04:18:50.704
+	thrust profile: [-3.7741093121961535e-8 -2.6257971335176648e-8 -2.1606384855810645e-8; -2.1363083523959785e-8 -4.234571308044473e-8 -8.269824340036801e-9; -1.7179727443085232e-8 -4.817903392853783e-9 1.1405733095493886e-8; 6.543773827193354e-8 7.63399812774497e-8 3.918240890364693e-8; 1.3414420888442994e-8 1.4060087327107107e-8 -8.242716667432803e-8; -1.8088388278070475e-10 -4.1359611682043475e-10 -9.03470171888568e-9; 4.3064264083954854e-9 3.2442366380236367e-9 -1.598356883588943e-8; 3.261934834405667e-8 6.450483621536437e-8 8.2007353416575e-8; -1.7993125019529573e-8 3.862145335097065e-9 5.231141768695811e-9; 2.5346874206765178e-8 2.0165133642770633e-8 5.961057304477184e-9; -1.8904868856526572e-8 -1.201092354618878e-8 -2.4170378084370648e-8; -1.1110813643371359e-8 -9.930972424447597e-9 -2.2310217231961474e-8; -2.3010965850571813e-8 -4.590923869358927e-9 -5.082758311888812e-8; -1.064446394813755e-8 -1.6835335671720645e-8 -4.524794179174139e-8; 1.6919283931076332e-9 2.0866300176185552e-9 -1.1111279350528446e-8; -4.352351680251087e-9 -5.215082497858078e-9 -1.2228449319478551e-8; 6.0054113300816905e-9 -7.05448971432868e-9 -5.6941027568265595e-9; -1.951082125424566e-8 1.1499547353566501e-8 -5.019589935213733e-8; 1.197134200084507e-8 -2.127430780809517e-9 4.800535709688631e-9; -1.311850186946498e-8 2.508766374053081e-8 3.5397163567430844e-8] %
+
+Mass Used: 7.579702014481882e-6 kg
+Launch C3: 34.82958605340684 km²/s²
+||V∞_in||: 0.8130770396493041 km/s

archive/EM_3-29/EM_2022-03-29T22:58:44.883/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:58:44.883/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-14T07:05:59.170
+Launch V∞: [1.6949045581275466, -1.1749158457323354, 0.4459844940604056] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [0.2807404173223861, -0.5148397948760617, -0.024574238754993954] km/s
+	V∞_out: [0.4816521199334624, -0.31105824990728403, 0.021223537272540942] km/s
+	time of flight: 1.0181159999765144e8 seconds
+	arrival date: 2026-07-05T16:05:58.170
+	thrust profile: [1.4156868146913603e-5 -8.937824771836181e-6 -1.4258721529256393e-6; 6.201501805968712e-6 4.891054084739865e-6 -2.4147768084891413e-5; 8.710377800639082e-6 -2.5247715656786118e-5 -4.228464809233087e-5; -5.49592858423698e-6 -5.956986519709633e-6 -6.0003598197038516e-6; -2.2049093171105036e-6 -2.489010425867444e-6 -3.9225913222362265e-6; 2.1078914306123458e-5 -1.1944173566312533e-5 1.8244198561717057e-5; 1.9561991087389005e-6 -1.1752657963774734e-5 1.683487450213938e-5; -6.055159240369156e-6 -2.206637657527475e-5 1.5277910735365964e-5; -2.1063568637137504e-5 1.0199794653949234e-5 -1.0165697723410959e-5; 0.0006945866286583284 -4.8718537131140276e-5 -0.0010004798714153944; 3.549819219472579e-6 -5.173787731590263e-6 -8.794510883495692e-6; -1.1187037009877784e-5 3.9873466996776687e-7 -1.2842230899218392e-5; 1.819371322436169e-5 -1.985114604615626e-5 7.40305445774715e-6; 4.351771410931808e-6 -1.2633771406394241e-5 4.02517242765969e-5; -0.00021811083392391314 -0.006360908650050679 0.007451776526230452; 0.4683451802604527 -0.7651039839559246 0.09069086407503833; 0.8713044694433868 -0.27831401933737787 -0.20462753606922815; 0.012344351227493076 0.0030669853424402133 -0.014728214668807213; 6.768683876914276e-6 7.65498676530381e-6 -2.3634699931764597e-5; 5.463932969042515e-8 1.6589754704890928e-6 -6.114493334584618e-6] %
+
+Mass Used: 75.80031539540141 kg
+Launch C3: 4.452030874656779 km²/s²
+||V∞_in||: 0.5869234102647126 km/s

archive/EM_3-29/EM_2022-03-29T22:59:31.051/mission

@@ -0,0 +1,22 @@
+/home/connor/projects/thesis/archive/EM_2022-03-29T22:59:31.051/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-12-23T04:52:28.411
+Launch V∞: [-2.3721677208600336, -1.1471540814232561, 1.82724714241875] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [0.7657978493736273, 0.47268498190867225, 0.5669638080447448] km/s
+	V∞_out: [0.671344291602754, 0.7165876747149759, 0.4086328277033566] km/s
+	time of flight: 6.692110088878082e7 seconds
+	arrival date: 2026-02-04T18:04:08.411
+	thrust profile: [0.0008233730574660627 -0.0006089913686355275 -0.0003656792494954692; 9.277035119329392e-5 0.00018105994933842137 -0.00045064421020144603; -0.0009643656591043792 -0.0005295771327107068 -0.0003527133652685661; -0.0001829291084087302 -0.00028713103539127654 -0.0011612339233188311; 0.0002628094997902115 -0.00038049047451517036 -0.0004438420586700227; 0.00022847673868341134 -8.081668903608331e-5 -0.0004169573293423967; -0.00024469370633056417 -6.337239455279198e-5 0.0008380473882381952; 0.0007752101556583943 0.0006834443935228009 0.00015265143847038387; -5.4459788825500716e-5 -0.0014820986794018846 -0.0012653925633815618; -0.00021218967607504187 -0.00020847681093790597 -0.0002734855651715473; -0.00017082953277056904 -0.00011256508693154773 0.00152134489853549; -0.0007743596333968497 8.88770635961271e-5 0.001957585876424173; -0.0009465135793430943 -0.0008606487267644376 -0.000381605440474747; -0.002413182432020938 -0.0026073704810047824 -0.00027904268175806847; -0.0005254492375900773 -0.002157747734677348 -0.001799801241758866; -0.0005194698886906513 -0.001005331073405558 -0.0013843897937889358; 0.00048689741373146193 -0.001401700406807511 -0.0024375166130219906; 7.266464024313168e-5 -0.00033741672866423523 -0.0004478141428623512; -0.000586239166722991 0.00012793840622519977 -0.0009074360302595961; -0.00018809051058659194 9.565179941071708e-6 0.000633927457634841] %
+
+Mass Used: 0.7381269704351325 kg
+Launch C3: 10.281974301893808 km²/s²
+||V∞_in||: 1.0636378132897837 km/s