Additional display functions and section 6 draft done

2022-02-20 22:10:56 -07:00
parent 472662fb60
commit 700f7e28cf
169 changed files with 810 additions and 944 deletions
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+/home/connor/projects/thesis/archive/EMJS_2021-12-01T15:04:58.660/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-11-08T18:47:22.305
+Launch V∞: [-4.451427517503081, 4.380713257243984, 0.9509666906856978] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [-7.503625705871378, 2.9922534516224317, 0.3970744313528344] km/s
+	V∞_out: [-6.203985495450952, 5.1853077278089845, 0.19685948210225732] km/s
+	time of flight: 7.692258675246356e7 seconds
+	arrival date: 2026-04-17T02:10:28.305
+	thrust profile: [-0.05747333201815444 0.01458857211306159 0.01661972438571343; -0.07640520733942768 -0.0880498378588422 0.009291396823580423; -0.0642351947881695 -0.14583843433809482 -0.01174256444385774; -0.03591836428259514 -0.19097919421877213 -0.030455634296288725; 0.0014696729268849598 -0.21419745388390338 -0.046332000137257384; 0.043321837437152184 -0.23281386608467833 -0.057269006919827066; 0.08487576000339314 -0.23180733654869165 -0.06400789992534636; 0.12836076596832638 -0.2345880635860211 -0.06663468113711396; 0.16914897842720558 -0.2202670166100522 -0.06608715415000553; 0.20331848204335912 -0.19904198276368773 -0.06263191481516477; 0.23625994800571543 -0.18017227778817843 -0.057302223507679384; 0.26476916718248283 -0.15037417766839517 -0.05026099494873699; 0.28150073209231896 -0.11974625587737671 -0.04226763198923683; 0.2911151952723726 -0.08935809631597122 -0.032922957893997004; 0.29662192049119385 -0.05630987736862665 -0.023018382921682446; 0.3163317621362404 -0.01253021176722935 -0.013235490847343547; 0.25582892879782015 0.03994726547045516 -0.0012262871620623078; 0.20630604157449897 0.09278869993819255 0.011047803244751797; 0.13239326442164706 0.18510472327622382 0.022309378373958296; 0.0678407381537921 0.24416553319280734 0.027187329287448894] %
+Phase 2:
+	Planet: Jupiter
+	V∞_in: [-2.4066983016171593, 3.60782547580802, -0.0729666504902062] km/s
+	V∞_out: [2.378938038105792, 3.622859356538288, -0.17162450321036135] km/s
+	time of flight: 1.0365627669349712e8 seconds
+	arrival date: 2029-07-29T19:35:04.305
+	thrust profile: [-0.08661540144522925 0.5452498417652726 0.01940681405322532; -0.3026836754787113 0.3296518390803253 0.005983402538334351; -0.3406876005629003 0.11833095428025397 0.003356530625833691; -0.2835305485605863 0.05826412825528092 0.02255167620704516; -0.2312925636505238 0.037264277244941184 0.05388961098566991; -0.18711959340793846 0.02248626525242582 0.07873824296078222; -0.1586634246283703 0.009933258699574466 0.0871013968397894; -0.13480225405151802 -0.0016459373751799647 0.08376814481354339; -0.11717491300808694 -0.011644771387652143 0.06591943652720958; -0.12385446642299068 -0.021486105366059834 0.04559099694744897; -0.09388047865743618 -0.028093190404018073 0.021912607207877112; -0.08329274681397837 -0.03442999409177474 0.004671009919336775; -0.074293683492257 -0.039542791582250804 -0.005853738709231158; -0.06633940754759032 -0.044531789384190786 -0.009552210711090501; -0.05819808497253237 -0.047725452096228235 -0.008621886584541672; -0.052136936558275115 -0.0524395749605876 -0.002738982045574738; -0.04346694186008132 -0.0559411143833451 0.005899905372803087; -0.019037945479989642 -0.06356156997525016 0.022900432372144015; 0.03382392128782208 -0.03750155602427737 -0.01509909397132852; 0.0372737888254289 -0.03393228709124474 -0.008856011117644847] %
+Phase 3:
+	Planet: Saturn
+	V∞_in: [-1.348151617130741, 3.372644961627469, -0.15974064227398158] km/s
+	V∞_out: [0.5003596890905858, 0.5035022711921476, 0.4902757482488732] km/s
+	time of flight: 2.6430663321089447e8 seconds
+	arrival date: 2037-12-13T22:05:37.305
+	thrust profile: [0.09042797681998876 0.08185621600988492 -0.005657240382538273; 0.08801730768503421 0.06654785786786777 -0.005370519173262853; 0.08823193892876004 0.06301303625131692 -0.005301669247083464; 0.09786240449059495 0.0767776838916466 -0.005515040644430515; 0.08471215842112331 0.09323975234752191 -0.004395184816667355; 0.06296777251631458 0.13453925938779707 -0.0025772294050847586; -0.0014186632217062752 0.15454606073890062 0.000798883942976955; -0.06382656189096726 0.14369239243391718 0.004139373253375935; -0.09924285361658083 0.11731937511826053 0.006398669227156636; -0.11580556499542272 0.09241219909488727 0.007641311131976814; -0.12704630471212713 0.0755704468000314 0.008542821687616114; -0.13059068423655953 0.05648447252052886 0.008518267583078705; -0.1375065378923194 0.029657327876499343 0.007947474105719379; -0.12731258715678567 -0.013661649213132244 0.005928368352642089; -0.08615459629776862 -0.051365993070702234 0.003434419522338479; -0.06064751058410859 -0.050519207115431015 0.004480131985829094; -0.004983547686528498 -0.05050727346302307 0.028470779024005587; -0.029138511656783765 -0.04657877128192993 0.022486478212922927; -0.035824958961586245 -0.02656318094078993 -0.022032681036760468; -0.042164309076524915 -0.03952915140222731 -0.007355989451236212] %
+
+Mass Used: 537.3508733080857 kg
+Launch C3: 39.91019323257055 km²/s²
+||V∞_in||: 3.6356242782715444 km/s
@@ -0,0 +1,29 @@
+/home/connor/projects/thesis/archive/EMS_2021-12-12T16:01:04.514/mission---------------------------
+
+Spacecraft: mySat
+	dry_mass: 200.0 kg
+	specific impulse: 3200.0 kg/s
+	max_thrust: 0.00025 kN
+	num_thrusters: 1
+	duty_cycle: 1.0
+Launch Mass: 3500.0 kg
+Launch Date: 2023-07-08T05:11:21.442
+Launch V∞: [7.608076212455678, 2.807333338029972, -0.7296465923907695] km/s
+Phase 1:
+	Planet: Mars
+	V∞_in: [8.010347423561068, 3.2469372890009143, 0.9052053694493565] km/s
+	V∞_out: [8.595491836222386, 0.9305961590076297, 0.8829460767922697] km/s
+	time of flight: 1.285682951483629e8 seconds
+	arrival date: 2027-08-04T06:36:16.442
+	thrust profile: [0.07414876190498018 0.061418074622027974 -0.012644930305191268; 0.005288427050926843 0.06622341067027271 -0.01948043031768979; -0.03963858081578733 0.046911280729787376 -0.025333966766685957; -0.0693496161126329 0.031308343596909594 -0.035395597569043105; -0.09403908126205902 0.015893237291132945 -0.047093551884514924; -0.12169201205925062 -0.0007977301725099221 -0.056349298411649505; -0.13903080782532432 -0.023716664620632603 -0.06390511581051783; -0.15450668610406254 -0.04110038684733795 -0.06471664925953435; -0.15811658018787572 -0.056770227221372115 -0.06186158450863763; -0.14688366879113826 -0.06858393095838325 -0.048462199618237715; -0.12668694389924282 -0.08632300225726315 -0.034758267139006545; -0.10530920293607691 -0.10528354810684375 -0.02720399752175047; -0.09090371755012416 -0.12194843310927922 -0.021454466137421403; -0.07844574463506924 -0.1363037266093477 -0.01574716544865601; -0.05844360196093202 -0.1515941613574019 -0.009255165942420979; -0.034312300204900524 -0.16511832855603034 -0.0009688494952381404; -0.0028992408640754097 -0.17347460518323504 0.006524027611181451; 0.03968790735981553 -0.17103970596354526 0.01802812299096526; 0.09266705743272931 -0.1535778429859241 0.025140107388620526; 0.20165971230655427 -0.14421264141271573 0.040991785807895254] %
+Phase 2:
+	Planet: Saturn
+	V∞_in: [5.172452466285559, 3.681404565790302, -0.7376128757432779] km/s
+	V∞_out: [1.0471838805707034, -0.9458496802640074, -1.0540623554828816] km/s
+	time of flight: 1.3794018891807556e8 seconds
+	arrival date: 2031-12-17T19:19:24.442
+	thrust profile: [0.4631902795092741 -0.08224771535152973 -0.006480928889750821; 0.41704341820262636 0.21095659271139136 -0.02620914649646857; 0.2797622883993905 0.28592479641588525 -0.047115859690752125; 0.16999303712128083 0.27059720181308317 -0.05726221774165335; 0.10505343297735933 0.24439744913692196 -0.06242988174728664; 0.06300675973086067 0.21817544269642067 -0.06368113246047818; 0.035798514967212466 0.18835657288959481 -0.06877313709544629; 0.01319570173604884 0.17195586849080916 -0.06353926803226635; -0.0028206814647056726 0.15245841060553408 -0.06090532235092303; -0.015082533306159574 0.13455720233249788 -0.058050722168487584; -0.02467540253289453 0.11876086660610821 -0.054811640710621876; -0.03294606177558641 0.10466484376452906 -0.05156606010332461; -0.03552225607407402 0.09449768203449549 -0.04909814885511831; -0.044198382979974346 0.08219311436910662 -0.04488660247693665; -0.05192427793509353 0.07124227028180148 -0.0429911500566686; -0.06297039751477762 0.0597152997307626 -0.041771291047482936; -0.07719329504107608 0.04574422574176853 -0.04069542662253849; -0.09549593365185864 0.02256061596005478 -0.03696703906940773; -0.1044144745168432 -0.01480076697580528 -0.01798772858528922; -0.10164225283033314 -0.03637354833556879 0.00015260443811211083] %
+
+Mass Used: 369.23128366753645 kg
+Launch C3: 66.29632827513589 km²/s²
+||V∞_in||: 6.391484713856986 km/s