Files
thesis/archive/ES_0.5648804830164132
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5648804830164132---------------------------
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: 2023-04-28T01:10:36.355
Launch V∞: [6.03152771952163, -7.3783041874024455, 0.06059433318194016] km/s
Phase 1:
Planet: Saturn
V∞_in: [6.860035792258668e-7, 4.639804106011067e-6, -3.103847947076007e-7] km/s
V∞_out: [1.745173560922323e-6, -3.7933211873294417e-6, 2.157888553506153e-6] km/s
time of flight: 1.874957778739016e8 seconds
arrival date: 2029-04-06T03:20:13.355
thrust profile: [0.6212419395332285 -0.11949501495796519 -0.145550881865982; 0.2227583447691549 0.09294000375670287 -0.16287679457780707; 0.1029087216356881 0.07829247412476015 -0.13046173563649982; 0.06976872822128206 0.07301143728134825 -0.12637962572496975; 0.04856421820472052 0.06388309454514603 -0.11642646717890474; 0.04965326437083251 0.07883587553113089 -0.1474458126796992; 0.014870707927135931 0.02623461443587498 -0.05379250155127336; 0.007518129415447085 0.01511819977085026 -0.032991280058931365; 0.0025826601163650206 0.0060070855838330805 -0.013487252476972108; 0.00024601604323005755 0.0005114362206548856 -0.0012215066409381671; 0.00019534778030919542 -0.00016508842086034438 -0.0001433433474508182; 0.001248774106875504 0.0032725705261738955 -0.00747386743725113; -0.0001847730715148254 0.00047391875758385024 -0.0009108680580054125; 0.0004079439922884899 0.0005272681416763655 -0.0008353617969207596; 8.595515514513518e-5 0.0002908406866422562 -0.0007693596409539824; 5.489695896287448e-6 0.00010009764449052295 0.00015511746131804645; 0.0005456328574027394 0.00018144915764139866 -0.0003172973211890193; -0.00014300435889761694 0.00018435644442035002 -0.0007395666201116901; -0.00026488345549786435 -0.00032829930171487064 0.00042141141530593147; -0.00041396886296680524 -0.00021054495100375525 -0.00030423908178343667] %
Mass Used: 129.23006609841195 kg
Launch C3: 90.82237098641203 km²/s²
||V∞_in||: 4.700502289506254e-6 km/s