23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5626885828880006---------------------------
|
|
|
|
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: 2023-05-02T18:48:47.362
|
|
Launch V∞: [6.578286677288327, -7.428225469099222, 0.08789394197401422] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-2.3433498402186928e-9, -2.527972012235456e-10, 5.544058557540606e-9] km/s
|
|
V∞_out: [-9.404559336577544e-10, 2.154229139508857e-9, 2.988293583493382e-9] km/s
|
|
time of flight: 1.874957778744414e8 seconds
|
|
arrival date: 2029-04-10T20:58:24.362
|
|
thrust profile: [0.19087812033288282 -0.051274268314865847 -0.07439458016983722; 0.05200725770368752 0.011887451675131179 -0.06344669893749036; 0.051354056041595875 0.023080623319738036 -0.10463795979233187; 0.05145976499039695 0.03079572421138714 -0.14552564989325503; 0.04675688586884377 0.0332487783963554 -0.16850350699592348; 0.020606723552495203 0.016440256083553626 -0.09230267853389425; 0.013197180569930432 0.01134420422742778 -0.06983710843879155; 0.010632725498596047 0.00979669973633893 -0.06420101735924781; 0.006499916665214373 0.00675625199612968 -0.04762379608405519; 0.0018185160621109666 0.001091530295265652 -0.011503245378027965; 0.0042217890694666044 0.004230757701879753 -0.030228307417786947; 0.00029533760457097304 0.001240773713608102 -0.007508855674116313; 0.0014597083431440142 -0.0021145642663299427 -0.0006597988434185503; -0.00027071882768356045 -0.00033091152584336346 6.514674524533363e-5; 0.00030551050137569925 0.0006880254431251894 0.0009105415379046459; 0.0006145111791109417 -7.30789339819266e-5 0.0018385602350685214; -0.00032305777483547765 -0.0020954241138625603 0.002100097546888631; 0.0024930307326671963 0.00020537038353843546 0.006731674614516139; 0.00043987612508814434 -0.0006396652600486325 -0.000931312059599365; -0.0004385849918649682 0.0013641402496890214 -0.0007071168997197363] %
|
|
|
|
Mass Used: 82.11934502450549 kg
|
|
Launch C3: 98.46011457339918 km²/s²
|
|
||V∞_in||: 6.024265945991981e-9 km/s
|