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thesis/archive/ES_0.626461838062805
2022-04-18 10:59:25 -06:00

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archive/ES_0.626461838062805---------------------------
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: 2023-04-25T08:46:59.976
Launch V∞: [5.598203708452922, -8.055060790956134, -0.4092056810853797] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.0005328101729173673, -0.0003546547452760865, 0.0002672949268688542] km/s
V∞_out: [-0.00035161227560696277, 0.0005016955608288436, -0.0003267989793541001] km/s
time of flight: 1.5443839936675316e8 seconds
arrival date: 2028-03-16T20:20:18.976
thrust profile: [0.37706053505999043 -0.193462617493502 -0.160870965263036; 0.05938234517589861 0.0023623445406309954 -0.05300847385179309; 0.09978065540289405 0.019956869063596817 -0.1571730595632127; 0.10625809107929994 0.034319122389059126 -0.2324530187168348; 0.06769096782760659 0.02684274557757831 -0.1762202435358548; 0.02985911454677757 0.01626200802224529 -0.08719435261798747; 0.04474482299925178 0.02196548074925249 -0.16722950991396113; 0.012775721674512196 -0.0067312333485375665 -0.043166239881520414; 0.029081163212316123 -0.019057231681223308 -0.07764752718671836; 0.020586113126807755 0.006701106166532529 -0.03254685456070806; -0.017316126322667467 0.01966559520848256 -0.012873179123236978; 0.0519763635966074 0.0035344120755091014 -0.05450752382016304; 0.029619327121220534 -0.01443454368144384 -0.06781704629883452; 0.019527365045497434 -0.07542755837260648 -0.013867769893992975; -0.07513400554552445 0.04114682592508424 -0.08571562048052853; 0.13672372471658567 0.015614860083181328 0.0035423907712768335; -0.1250401159877621 0.10930440219093122 -0.0726313790849129; 0.019827213404346507 0.013376661963941645 0.14988691879793342; 0.01744810976137554 0.015737877997633303 0.1559502178777067; 0.013765039827757416 0.01835605356031152 -0.12413591622366017] %
Mass Used: 168.58933709212897 kg
Launch C3: 96.39133839676745 km²/s²
||V∞_in||: 0.0006936232742929744 km/s