Files
thesis/archive/ES_0.5632924724725766
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5632924724725766---------------------------
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: 2024-05-14T18:16:58.711
Launch V∞: [7.989738362559125, -5.893713193889766, 0.020867267096024385] km/s
Phase 1:
Planet: Saturn
V∞_in: [3.427345033296749e-8, -3.569489341029126e-7, 5.853866869694083e-8] km/s
V∞_out: [-5.7036796893320146e-8, 2.114713711424689e-7, 2.9011574788615807e-7] km/s
time of flight: 1.8199201736375532e8 seconds
arrival date: 2030-02-19T03:37:15.711
thrust profile: [0.1910268681095348 -0.013776957005154186 -0.07032054397193149; 0.04712474244058465 0.019115649718153677 -0.06080432574918376; 0.052706953446937134 0.03214493936013512 -0.11131387962810936; 0.04180806786537722 0.03193170738556777 -0.12723520228712015; 0.029386995106262914 0.02614794844167848 -0.11935965904908064; 0.023230566902550237 0.022222835783333172 -0.11559028630323116; 0.010367890923284892 0.0112185517710169 -0.06281633884691362; 0.006311203978362441 0.007580482219486143 -0.050111610261398876; 0.004367777706530728 0.00656631160188738 -0.045581697940741024; 0.006531565284192075 0.008554169647194172 -0.05813715795094419; 0.0019478372448409674 0.002242995512819619 -0.019211762300047952; -0.0008965664328833561 0.010450968504001179 -0.0012775021228759193; -0.0024003211071949113 -0.00530488599631238 -0.0038565062326399975; -0.00467214615207885 -0.0009879086853769193 0.0027773829985342927; -0.00013409872665568216 -0.00012961744231171823 -0.0020333708169290848; -0.0015847415485975849 -0.0015256729391131985 0.0069420506995536615; -0.0007639337030767271 -0.0003590877806199952 0.002046575023638874; 0.00042854269884923116 0.017252140472675252 -0.0006944772517102301; -0.022083810892091764 -0.0007780750540864914 -0.01324558614548058; 0.0092786675913685 -0.019522836037527858 0.0026852089101102538] %
Mass Used: 82.16999430324995 kg
Launch C3: 98.57220975681534 km²/s²
||V∞_in||: 3.633372905273309e-7 km/s