23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5670667038231234---------------------------
|
|
|
|
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: 2024-05-09T05:54:42.921
|
|
Launch V∞: [7.438360340212719, -5.893807377906329, -0.06450452205271918] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.01658124652414911, 0.10190364244063732, 0.12570841253676115] km/s
|
|
V∞_out: [-0.06780909108935346, 0.05744323073110756, -0.1366167008743838] km/s
|
|
time of flight: 1.8749577787307426e8 seconds
|
|
arrival date: 2030-04-18T08:04:19.921
|
|
thrust profile: [0.4951182466214266 0.023574147506026745 -0.08349736518065393; 0.37255102100186943 0.25584925640465894 -0.20256030811457792; 0.12481818800313123 0.16681740090116148 -0.14219140597251495; 0.05634839587353808 0.10777132188253934 -0.1073815169314239; 0.05437987287729945 0.1360986901427992 -0.14300087325936642; 0.007182465236308588 0.024267873380192553 -0.029251672064120878; 0.01992117754121125 0.09196940720550725 -0.10917491560275684; 0.0011506763274736049 0.0042983597632887515 -0.005092072532471246; 8.702535681573122e-5 0.001204790368388517 -0.0016618812401853135; 0.0004968194183818163 0.0028661174010601903 -0.004346316386634564; 0.0007443380308066334 0.00024077896844668415 -0.0007460126696798791; -0.000457567850602181 0.00020083151409528756 -0.0010796419022913743; 0.00011350769522722149 8.368189547504855e-5 -0.0004495048129331195; -4.332909043228719e-5 -0.0001845141533061354 0.00023384411205319033; 3.909558972757098e-7 -0.00012776250728420424 0.0004332320888308945; 0.0002280628834258471 -6.429922487301648e-5 0.00046093897193398765; -9.441233644452577e-5 0.00024002799068157277 -0.00042797663111476385; 0.00034275378804533743 0.0013804801602371188 -6.290898408782498e-5; 0.0013312368772176665 0.0012410177656036966 -0.0007569608192420604; 0.00012887760023242833 0.0016419629343101794 -0.0009911285662667427] %
|
|
|
|
Mass Used: 136.16755817319017 kg
|
|
Launch C3: 90.0703307920778 km²/s²
|
|
||V∞_in||: 0.16267112546938498 km/s
|