23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5668679347285605---------------------------
|
|
|
|
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: 2024-05-21T08:40:24.407
|
|
Launch V∞: [7.87124946065423, -6.264946181573107, -0.3696032474917886] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-7.026071513725205e-7, 2.234642109311443e-6, 6.789353178143177e-6] km/s
|
|
V∞_out: [6.497921263478018e-6, 7.196655839257399e-7, -2.9956076973378556e-6] km/s
|
|
time of flight: 1.8749577779600278e8 seconds
|
|
arrival date: 2030-04-30T10:50:01.407
|
|
thrust profile: [0.16184731336408406 -0.002630535080258912 -0.0668773814114606; 0.06932527173223155 0.03295407108734363 -0.09715444031399487; 0.029554066870157828 0.02073904918592164 -0.07687275744646768; 0.02403801644619919 0.021832732910814775 -0.09018264014092857; 0.020986960199780667 0.02207468224814829 -0.10241348270217149; 0.01223029613258797 0.015979895289686467 -0.08104195046384526; 0.01079775587561704 0.014987564314246098 -0.086173843405933; 0.010038297388308446 0.01262971926312931 -0.08382256075499199; 0.0038506636335487584 0.004416628060867883 -0.03446267879675697; 0.0027326156397775624 0.0029882057290727495 -0.026810411046016957; 0.0025137452705131917 0.003080325872985221 -0.027213725834879843; 8.664159412433565e-5 0.00023735854925145168 -0.0005547843267518954; 0.00014180834279252833 -0.0002736880724670454 -0.0004309595192277216; -0.00016659344769417712 5.0427542931759755e-5 0.00041930912717516263; 6.678237411382709e-5 5.708027033238284e-5 0.00018643673818477153; -0.00045899113450067466 -0.0002919493767015868 -0.0010080919346408983; -0.0009398610869794418 0.0007454469983722585 0.00034006084636375295; 0.0010766514180172216 -0.0007991512411292596 0.0006223345253021092; -5.834267020668712e-5 8.168460764432974e-5 -0.00023247496999206582; 0.0007879698169520399 -0.00012467163122551833 -0.00047479941903596525] %
|
|
|
|
Mass Used: 70.18002632257549 kg
|
|
Launch C3: 101.34272529041344 km²/s²
|
|
||V∞_in||: 7.182102668677925e-6 km/s
|