Maybe nearing the final commit

archive/saturn/ES_2022-04-02T14:30:27.910/mission

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+/home/connor/projects/thesis/archive/ES_2022-04-02T14:30:27.910/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: 2023-04-30T10:42:53.737
+Launch V∞: [6.471151295328684, -7.370093125495227, 0.1471444087176648] km/s
+Phase 1:
+	Planet: Saturn
+	V∞_in: [0.0011016712208284018, 0.001193317665709545, 0.0011284459950617813] km/s
+	V∞_out: [-0.0013212882247491697, -0.0006402618783858693, 0.0013249649980667188] km/s
+	time of flight: 1.8586551451242688e8 seconds
+	arrival date: 2029-03-20T16:01:27.737
+	thrust profile: [0.34816593202635143 -0.09016300532970822 -0.11984880840754134; 0.060934867329879086 0.015900377772554663 -0.06439542879673578; 0.05633720205505469 0.028914725747037226 -0.0996495075588441; 0.06330666013244533 0.04409491325404843 -0.15633154563783136; 0.0394194911156743 0.03303344724606148 -0.1252177975024216; 0.03234762325404856 0.03136698447248268 -0.12511375359960542; 0.03154342715128428 0.034121568693792986 -0.1437825111683027; 0.008289385990413433 0.009595068731611724 -0.04427632783857093; 0.002136247718622523 0.001470160769050456 -0.012444247342867514; 0.0018093799205720644 0.002089387539433632 -0.010912883437983656; 0.0002760205068699395 0.0002984621041452654 -0.002059210160487663; 0.0004273343871331427 0.0006087053409058076 -0.003795471399462705; -0.0001799331844267571 0.00012037796986719939 -0.00024659503854662103; 0.00013990951839967919 -0.00029575557397248453 -0.00011257990744582862; -0.000614150557542183 0.0008502168982850079 -0.0003376355670288909; -0.0008804534336335694 -8.269349664778052e-5 -0.000632456517603454; -0.0008316974334143153 0.0003135027300336823 -0.0004726228836000578; 0.0005727975202778207 0.00044876254245158876 -0.0005711028042968798; 3.62608887044046e-5 0.000582228987042213 -0.0015471075290508958; -0.00015234799294315781 -0.00025744481686610667 -2.9842734467018593e-5] %
+
+Mass Used: 93.53064646715393 kg
+Launch C3: 96.21572324252298 km²/s²
+||V∞_in||: 0.001977644278900276 km/s

archive/saturn/ES_2022-04-02T14:43:26.363/mission

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+/home/connor/projects/thesis/archive/ES_2022-04-02T14:43:26.363/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-04-30T19:57:56.612
+Launch V∞: [6.405474755176122, -7.3900240973677365, 0.06380150742647996] km/s
+Phase 1:
+	Planet: Saturn
+	V∞_in: [8.845477174913946e-6, 1.1595633238974296e-6, -2.53958525884217e-8] km/s
+	V∞_out: [-1.7215228302243153e-6, 3.8729325339638874e-8, 8.733327905166755e-6] km/s
+	time of flight: 1.8749577788724747e8 seconds
+	arrival date: 2029-04-08T22:07:33.612
+	thrust profile: [0.3532736189291979 -0.07957696996168889 -0.11573193739758812; 0.0739878629979336 0.02295380224798903 -0.07498400660525116; 0.09168090432856428 0.05432801353413295 -0.15285608888607036; 0.08574086950319204 0.06910585053670845 -0.19999338233636935; 0.0400414422201257 0.03875100333070956 -0.12229237709629778; 0.03258259202158226 0.03713578481743383 -0.12353513268560726; 0.012417336611257972 0.01556828980981476 -0.057033084437855104; 0.0025701620442923167 0.003718201910167825 -0.01419424338655812; 0.004068375950339169 0.006413323665496442 -0.025558683158119714; 0.0010610872645670296 0.0018118064020934408 -0.0073979852498836755; 0.0007915074644420847 0.0014371710977416085 -0.006142894293848515; 0.00011693650669376116 0.00022769271601352848 -0.0003328552699521106; 2.4353713923558043e-5 0.00010628016125793987 -0.0005927137301198118; 0.0001354521898069056 0.00010303580217391736 -0.00039219057300311604; 0.00016523814905179804 -0.00016691610666035386 -0.0002590759639041915; 0.0001266361254982333 0.00015828576308795974 -0.0006156867198432335; 0.00023176672580329702 -5.9645489892740295e-6 7.850577957903819e-5; 0.0010552143660857304 0.0008665606653972042 -0.00030929641961722186; -0.0006290351415415637 -8.118343507894017e-5 0.0010639985232273105; -0.0009023532414626753 -5.706217596898628e-5 0.0012658257422519792] %
+
+Mass Used: 96.5319026649936 kg
+Launch C3: 95.64663363122433 km²/s²
+||V∞_in||: 8.921193782413896e-6 km/s

archive/saturn/ES_2022-04-02T14:59:19.235/mission

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+/home/connor/projects/thesis/archive/ES_2022-04-02T14:59:19.235/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: 2024-05-14T07:57:24.826
+Launch V∞: [8.1332663571246, -5.661986515759155, 0.22766044177874376] km/s
+Phase 1:
+	Planet: Saturn
+	V∞_in: [1.123340652251088e-6, -3.7330513819710547e-6, -1.0846981586769346e-5] km/s
+	V∞_out: [-1.0492432785177735e-5, -1.2239051288617402e-6, 4.687451703815964e-6] km/s
+	time of flight: 1.859737203924726e8 seconds
+	arrival date: 2030-04-05T19:19:24.826
+	thrust profile: [0.22943973812293017 -0.004893967763726286 -0.0801253153441409; 0.03144507004413593 0.016005514878668727 -0.039605355975015175; 0.039054529766301194 0.03197291138034155 -0.08689490156094459; 0.0378685260709824 0.04018324616401574 -0.12252200644008435; 0.02803090143364196 0.03535274273841469 -0.12081216327733243; 0.022471665512052253 0.032497625582222536 -0.12157198448109055; 0.01926878492754949 0.03153169051058213 -0.1281842797483311; 0.004043038254003434 0.0066904694410549765 -0.031175306636595977; 0.005131609501874749 0.009234170160377442 -0.04469930754406368; 0.0003470121363472272 0.0008038663204159477 -0.0038167565883837525; 0.00017609752178919131 0.00036474064628598307 -0.001954724463038849; 1.130336567161233e-5 -3.20909344426444e-5 5.0861087076908916e-5; -1.4439041978965607e-5 6.264510601075898e-5 -3.5503708158925043e-5; 0.00012451312434083361 -0.00034084972505136796 -0.0002481717343390714; -2.1043042384554106e-5 -9.974133023427434e-5 0.00022586203596731763; 3.0325725366321253e-5 6.145296121523383e-5 -0.0003832387995866655; -0.0002927026986088235 0.0007786944928326911 0.00012097830464324579; 8.96770273673005e-6 3.9333968087291074e-5 4.9980603904861806e-5; -1.0699601379404263e-5 -2.0172052201893303e-6 0.000372228156627312; -0.0002084346014800331 0.00032609368117262434 -0.0008865061071454217] %
+
+Mass Used: 74.69249898312728 kg
+Launch C3: 98.25994221732427 km²/s²
+||V∞_in||: 1.152625595695103e-5 km/s

archive/saturn/ES_2022-04-02T15:31:02.065/mission

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+/home/connor/projects/thesis/archive/ES_2022-04-02T15:31:02.065/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: 2024-05-15T00:58:50.661
+Launch V∞: [8.11320959943097, -5.645724124239646, 0.16747696452458005] km/s
+Phase 1:
+	Planet: Saturn
+	V∞_in: [-2.8516363421996975e-10, 4.096121164742909e-9, -2.0697877390789584e-9] km/s
+	V∞_out: [2.0790724859932675e-9, 4.127970936657118e-9, 1.0865120878585403e-10] km/s
+	time of flight: 1.874916083184456e8 seconds
+	arrival date: 2030-04-24T01:58:58.661
+	thrust profile: [0.2754868791323259 -0.004110502019187116 -0.09891196486261492; 0.04324638696098478 0.02247517183605698 -0.05675135816253204; 0.03892904890147251 0.03216852322138361 -0.09100809525201009; 0.03303057370015382 0.035080690423428366 -0.11279234928351167; 0.02181869863261611 0.025269776676374003 -0.09431813772381838; 0.0169559793237119 0.03232455050637029 -0.13374662433915915; 0.016111389795168594 0.023249907977486148 -0.09458558132535513; 0.007205435769196988 0.014290387230894463 -0.07630245560011156; 0.0015616439293485633 0.002593925533434509 -0.014198480084020042; 0.0006398647395756223 0.0011455341196065034 -0.0066362673778835824; 0.00021448383373943162 0.00048461036268397813 -0.0020121857045428612; -0.0005031708667670048 -0.0003846320758830172 -0.0002312837647398825; 4.666007485336052e-5 0.00010280240718190181 -0.000841627809911724; -8.908260282730824e-5 -5.559857473515914e-5 -0.0008097588799996763; 1.4481010457650478e-6 -0.00016875008215481904 -0.0011842708445230653; 8.682995627457883e-5 8.033742269629829e-5 -4.432971042893808e-5; -0.00029798252705925894 0.00034156180315709714 -0.0006198193274259149; -0.0003061369792923545 -3.25929632625721e-5 -0.0007753052016491007; 2.7198081862265237e-5 -0.00015657437876687814 -0.00016057616392290677; -0.0005144350151837572 0.0002711169996963231 0.0005113294575712331] %
+
+Mass Used: 77.59006675738965 kg
+Launch C3: 97.72641942496672 km²/s²
+||V∞_in||: 4.598211410905106e-9 km/s

archive/saturn/ES_2022-04-02T18:07:41.381/mission

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+/home/connor/projects/thesis/archive/ES_2022-04-02T18:07:41.381/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: 2024-05-14T21:35:13.618
+Launch V∞: [8.092028247187812, -5.690394550179761, 0.15870337020149677] km/s
+Phase 1:
+	Planet: Saturn
+	V∞_in: [0.007258340410626599, -0.004915549405160574, -0.0003090327712008995] km/s
+	V∞_out: [0.0063943921161191295, 0.0029021314271309787, -0.005208376883488668] km/s
+	time of flight: 1.8749577773970667e8 seconds
+	arrival date: 2030-04-23T23:44:50.618
+	thrust profile: [0.23623549046119796 0.001523213801416841 -0.0746418855277079; 0.04989778371798442 0.028557974139368027 -0.05866465575542369; 0.035473791749751 0.032507089227488954 -0.0752484296384085; 0.022627986747173957 0.026966919764486865 -0.07156789250913552; 0.04964790396262216 0.0738833298025964 -0.19559483393516622; 0.030631999959579347 0.05365872568512533 -0.15864114884262576; 0.00671793812371244 0.012495789298607023 -0.044004855933096255; 0.006194981641432508 0.01299461151504057 -0.04773667381981179; 0.0013970455272782531 0.0035097621778593085 -0.014148581638031872; 0.0014625087521359605 0.004576093171820035 -0.01812047518926974; 0.0003621287391874434 0.001192919920759847 -0.003924447420406894; 0.0003136102108716024 0.0009510767434047032 -0.003683238027775159; 3.55672194873085e-5 0.0002056947097665128 -0.0009531573613879192; -0.0002219678836028774 0.0002992512020633661 -8.263424581589065e-5; -4.180089723821831e-6 8.500643051220536e-5 2.6176105870720138e-5; 3.966745018590377e-5 5.7559670861396866e-5 -0.0004168195496730593; 0.0002960669240380866 -0.00015608457398720793 9.887024972396908e-6; 2.993253329593611e-5 -0.0001879527007887196 -2.49699959259209e-5; 1.3018003450243295e-5 9.194287517786575e-5 -0.00012566784156294738; -0.0002730423797779337 -0.0001543084966874625 0.0006099289590901544] %
+
+Mass Used: 76.50834802879126 kg
+Launch C3: 97.8866980497143 km²/s²
+||V∞_in||: 0.00877163797273837 km/s