Files
thesis/archive/ES_0.556453650248578
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.556453650248578---------------------------
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: 2024-05-14T05:19:12.896
Launch V∞: [7.900186867940902, -5.80195513699686, 0.10857680200473334] km/s
Phase 1:
Planet: Saturn
V∞_in: [6.947583884805263e-6, 4.0646650161173365e-6, -4.552817890949358e-6] km/s
V∞_out: [1.1518682539750074e-6, 9.164077841516948e-6, -4.0806772567926667e-7] km/s
time of flight: 1.8749577787492922e8 seconds
arrival date: 2030-04-23T07:28:49.896
thrust profile: [0.28442046836813084 0.013585284393893145 -0.08228666789852464; 0.14732123927234791 0.09862080801127338 -0.14168146984469707; 0.04240453031035516 0.045786027156268325 -0.08222227029211844; 0.03775120048006673 0.05745811298979494 -0.1105363034046098; 0.0451247977271028 0.09238869612463685 -0.18058723805956717; 0.013903954766717587 0.03228045561611711 -0.07402976841114384; 0.010306019683664062 0.03217604174662431 -0.0800549005101562; 0.0028140238716943063 0.010085338483080243 -0.026960908398847367; 0.000733011428638324 0.002632828992658677 -0.007770470082948786; 0.0005963431206027347 0.0026116461682093957 -0.007900661213048613; -0.0003542206865349215 9.043644330434186e-5 -0.00018519053804282536; 0.0004847976892110061 -0.00018052661237337038 0.00030540366720943824; -0.000785230044513999 -0.0003741287992273252 -0.0002682890107020895; 1.5881845965823356e-5 -0.0006549100921842162 0.0009395816081688684; -0.0002306124467296757 9.781665913671892e-5 0.0004646771881352666; 0.0003618486005749187 -0.0012214690212970871 -0.0010190122249592601; -0.0014053259199849585 6.431359687201566e-7 0.0006871368050395453; -0.0006030996248448406 -0.0006164324265606628 0.0010977859609292303; -2.9634007788058726e-6 5.605698929381583e-5 -0.00017705983945475321; 0.00022665715127808244 0.0005436971193447212 0.00019837296607864768] %
Mass Used: 88.6859468114194 kg
Launch C3: 96.0874248820437 km²/s²
||V∞_in||: 9.247625331824516e-6 km/s