23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5683800919173589---------------------------
|
|
|
|
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: 2023-04-26T11:06:20.567
|
|
Launch V∞: [5.8796980765685385, -7.699513759979515, 0.023779731897833185] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.8088982555167846e-6, 1.7932945155102162e-6, -1.2586487339165936e-6] km/s
|
|
V∞_out: [1.3736198361721747e-6, -2.847117718248814e-6, 1.6424158630393483e-6] km/s
|
|
time of flight: 1.7434908765969184e8 seconds
|
|
arrival date: 2028-11-03T09:24:27.567
|
|
thrust profile: [0.3437458772368016 -0.10052004608098333 -0.10256240161605201; 0.24561821767922581 0.06558217612712652 -0.19448485350281394; 0.1550782936085921 0.08610744684725716 -0.2027488003268019; 0.07297400265868532 0.05474394563438301 -0.13561173854176412; 0.0719396932222589 0.06744193429814727 -0.16808831016628592; 0.04753416682578699 0.051523608332406046 -0.1347393130495134; 0.019015592900381465 0.023044659568349498 -0.06444953384095302; 0.0061709765317855296 0.007839334369986248 -0.023398194689906875; 0.005071532813379796 0.001461738608706894 -0.011810214537064174; 0.00017237724148050002 0.0044006944408646175 -0.0033727731109086147; -0.0038424499983745453 0.002548113904661188 -0.005470469847870419; 0.003496468617774022 0.0026751949194425634 -0.012635290948949537; 0.002463043093126343 -0.001257930629711739 -0.0036231062379418126; -0.006463412282096785 0.002960007201126599 -0.0018933111937174565; -0.005491272727321873 -0.004801111971791273 0.0006521405855196688; 0.0014020454897180233 0.0008396388883575162 -0.007695522309112361; 0.0009521823951774992 0.0019426373605433529 0.0008053154011275427; 0.006320111421370169 -0.0018759837501903498 0.005487619617679176; -0.0012890380989360527 -0.003956173942469587 -0.008033517087961978; 0.003474930820786623 0.0014587177575956431 -0.010118261967396227] %
|
|
|
|
Mass Used: 115.62886589394566 kg
|
|
Launch C3: 93.85392708736681 km²/s²
|
|
||V∞_in||: 3.5623042071942847e-6 km/s
|