23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5681266851193401---------------------------
|
|
|
|
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: 2023-04-27T04:08:08.518
|
|
Launch V∞: [5.897907635291804, -7.6395801124006315, 0.08151378628158949] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [8.924568210827299e-7, 5.55152504343701e-7, -3.9045877055902735e-7] km/s
|
|
V∞_out: [3.5730387140972986e-7, -9.369660116246533e-7, 4.994857689633005e-7] km/s
|
|
time of flight: 1.737145165285222e8 seconds
|
|
arrival date: 2028-10-27T18:10:04.518
|
|
thrust profile: [0.5486694785915271 -0.1899935685034701 -0.1752381019970461; 0.09972415216727447 0.02169278600169451 -0.10186568430184313; 0.08166703732639337 0.03947918690774102 -0.13612296265826002; 0.12615892852337407 0.08555530620496503 -0.2584400357328541; 0.026042799813236137 0.02069743095967631 -0.07643900810513606; 0.02781757735255629 0.025559663347550228 -0.09771766198307504; 0.01730370346962114 0.01792118319143872 -0.0737008315503931; 0.013228285989473444 0.015242582641404167 -0.06524936846186037; 0.01338727312350569 0.01650892326797067 -0.07084485947607733; 0.004853458733934533 0.0064177217212504625 -0.029701232571989755; 0.0005294925322560747 0.0006593501971048405 0.00015554252131042652; 0.0034106058197031002 0.001514581018118541 -0.012540185268922255; 8.572005830546583e-5 -0.00040343881792471146 0.0014030737230490671; 0.00180096644377498 0.0032190177374379655 -0.004977403894504113; 0.0010274877053871884 0.0007166900214824088 0.0018741420266726065; -0.009026561069802779 0.00363842481256173 -0.0036464196746370217; 0.006271865944096209 -0.004295287718210693 0.0007090556368250255; -0.0028009892782466825 -0.010120737858850978 -0.00019389696606877515; 0.009889935098908037 0.0010463513902640206 0.007594552297941561; -0.007642357188291356 0.0019114779534010356 0.0018882827741150336] %
|
|
|
|
Mass Used: 119.4094635900451 kg
|
|
Launch C3: 93.15514326557457 km²/s²
|
|
||V∞_in||: 1.121218770839412e-6 km/s
|