23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5964101449058266---------------------------
|
|
|
|
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: 2023-04-23T15:36:12.945
|
|
Launch V∞: [5.572780505928083, -8.081080244275931, -0.3632695625181301] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [9.434681389051895e-5, -0.00011729639099541345, 2.17847520372116e-6] km/s
|
|
V∞_out: [2.6938536495178668e-5, -6.687638697199765e-7, -0.0001481138380764024] km/s
|
|
time of flight: 1.5020209292322063e8 seconds
|
|
arrival date: 2028-01-26T02:24:24.945
|
|
thrust profile: [0.35363518469169386 -0.1863585086957668 -0.15103546755776245; 0.13624494959029732 -0.0020161390311520364 -0.13917533725084746; 0.1100100268732051 0.023699593061482265 -0.16944790864712306; 0.10629342409101525 0.041195697369030525 -0.22295686066891013; 0.06424970214337128 0.026701707062407678 -0.17044602683118712; 0.04586993974969475 0.021262866461783547 -0.14376091218629533; 0.05299383958558698 0.029700816870782347 -0.1886820385955805; 0.025341374091532656 0.014282705353814776 -0.09926111730474754; 0.0023343460827907865 -0.0008272998021145036 -0.016641653861658143; 0.0049747999655983125 0.0017602619628351625 -0.0027412767573704233; -0.0010522655459844965 0.004810522815632512 -0.022361375608036436; -0.00963378379986123 0.007473672126207137 -0.00965863739817157; 0.0008059961157241137 0.00528272675155275 -0.015445829140486525; 0.033219252849465405 -0.03489551067220842 -0.0208485856807965; -0.037466553256678074 0.040120484283361076 -0.014655422716409983; 0.01333931848603116 -0.003220956477568987 -0.019036676169461638; 0.002288314898470265 0.020457086419450817 0.01861548521507564; -0.005350674161607055 -0.003958465601347505 0.028334046227197575; -0.009940998022594365 0.04538376961243448 -0.13901874353233531; 0.08608437546627436 0.0397912350815904 0.004768938608028814] %
|
|
|
|
Mass Used: 132.94355505920066 kg
|
|
Launch C3: 96.49170525673092 km²/s²
|
|
||V∞_in||: 0.00015054736924321977 km/s
|