23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5585199492799439---------------------------
|
|
|
|
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: 2024-05-11T16:21:44.985
|
|
Launch V∞: [7.838846546874048, -5.66360566090696, 0.33835335403093303] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0001788687454260667, 0.00014368369570958814, 0.00011655323677680784] km/s
|
|
V∞_out: [2.4617410139805725e-5, -0.00016325701272752838, 0.00019728632199514468] km/s
|
|
time of flight: 1.8749577786437747e8 seconds
|
|
arrival date: 2030-04-20T18:31:21.985
|
|
thrust profile: [0.4862175076940379 0.024922102972784792 -0.1141140125364418; 0.15006213374864277 0.10694254341732166 -0.1339616836603562; 0.064457366213566 0.07733436251569484 -0.11124631136708772; 0.04460401186045826 0.07153585115338167 -0.11777160428312237; 0.029183319133382398 0.06450823403539928 -0.11764742937330122; 0.010304237295103038 0.03141055580420059 -0.061795998690646343; 0.011889740755745856 0.04352427707983442 -0.0883758828543582; 0.0031376425758353533 0.01215283735821474 -0.028907490229156164; 0.002248946404348655 0.009241017243157392 -0.02211711626030574; 0.0006394606828607737 0.002850321403536122 -0.006490375898780988; 0.0010375775393478945 0.0012031089287276786 -0.001144509965639356; -0.0017178709938190549 0.0008565965706196191 -0.0007892514421859882; -2.4741867114297952e-6 -9.589686420087814e-5 -7.8968085195382e-5; -0.0013857877825612355 -0.0003055488105501825 -3.399805119396046e-5; 5.5223149231728005e-5 0.0017447491418039634 -0.00018520826525191274; 0.00033406333508363017 0.0004638454019863377 -0.0003871861106106545; -0.0003161496068389217 -0.0016444065145261853 -0.00035591147378056826; 0.0007333343103858653 0.0029057778304088767 0.0007334075700084672; -0.0007641269530156444 -0.0026903612897052256 -0.0013238927830175498; 5.029521136122758e-5 0.0035133188479505298 -0.0003823737538888209] %
|
|
|
|
Mass Used: 105.38244847729811 kg
|
|
Launch C3: 93.63842725988053 km²/s²
|
|
||V∞_in||: 0.0002573396384279173 km/s
|