23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.6177360477804267---------------------------
|
|
|
|
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: 2023-04-23T20:40:05.023
|
|
Launch V∞: [5.32800386919152, -8.721615038110999, -1.5386711729939877] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.022001281938764935, 0.01452195637843137, -0.0006928857666292247] km/s
|
|
V∞_out: [-0.007199905481891024, 0.0001139439554223504, 0.025379786728415024] km/s
|
|
time of flight: 1.1321333703795792e8 seconds
|
|
arrival date: 2026-11-24T04:49:02.023
|
|
thrust profile: [0.39195911532356914 -0.297584847505946 -0.23398349598689794; 0.26367086063144385 -0.057254032155884184 -0.28927418857371706; 0.1787210135708474 -0.0024815619765578517 -0.28577880223492547; 0.13047899910407748 0.013234079282670376 -0.26304667721247094; 0.08500057783555748 0.014136778957571651 -0.2074377920397077; 0.055360835530066765 0.013002309160187681 -0.14464018669771764; 0.036863164285305464 0.0084182165166477 -0.11409197961797127; 0.017356213812729962 0.004909359424314802 -0.059276778742835996; 0.0006982461460463465 0.00021511746707475357 -0.0030858781045980236; 0.003566316721079822 0.0010958589064471887 -0.013609681179807435; 0.0006109188822021932 0.00043418525813261393 -0.0011681150762362592; 0.0005527525633691365 0.0011522467118801206 -0.004242377721398292; 0.000408982821502114 0.00042799037730284527 -0.001304509074089614; 1.337675687972914e-5 0.00029714339388308976 -0.00045516952702224947; 0.0002070923121884598 2.0846265571404423e-6 -0.0005075988038644952; 0.000346516271540871 8.680207755398925e-5 -0.0016048649276752453; 0.00042581754109984743 -0.0009260197567012235 0.00017880102219947243; 0.0006198410649167242 -7.917324923935938e-5 -0.00035626621993844814; -0.0001550471399666102 -0.00016273933459518106 0.0001882147914257159; -0.0011072542695134838 -0.000542068755377877 -0.0001662390000981887] %
|
|
|
|
Mass Used: 97.56545443376035 kg
|
|
Launch C3: 106.82170308172643 km²/s²
|
|
||V∞_in||: 0.026370887635642548 km/s
|