Files
thesis/archive/ES_0.5605139576423932
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5605139576423932---------------------------
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: 2024-05-08T18:16:48.736
Launch V∞: [7.434238598358346, -5.933521765627251, 0.32522610065822943] km/s
Phase 1:
Planet: Saturn
V∞_in: [-3.21438616798795e-5, 8.705880350250296e-5, 0.00023771000796101187] km/s
V∞_out: [0.00023418504743583638, 2.7522886576570484e-5, -9.549932961836217e-5] km/s
time of flight: 1.7791101462638006e8 seconds
arrival date: 2029-12-27T22:00:22.736
thrust profile: [0.7504719725208537 -0.040959988155545995 -0.15509799737985513; 0.1185191714130535 0.0679961039417579 -0.10300058085330145; 0.1264374506334153 0.12250173205599602 -0.18766229033667772; 0.06662731543720393 0.08835459588522226 -0.15139498980584856; 0.04804751449256496 0.08042386328852101 -0.14890566327178625; 0.018075750289813855 0.035886408474172224 -0.07456631297148755; 0.013603804004789034 0.03240409118552923 -0.07113169491021608; 0.0028299772216219526 0.007852807993993145 -0.018732950225302913; 0.000674414139204634 0.0021682519400228286 -0.0054687146482979305; 0.0006945373563929057 0.0025920919536835847 -0.006790687638876995; 0.0004280404311632695 0.0017327790941959686 -0.004571926177987283; 8.845922417174818e-5 0.0006457546304282601 -0.0015085396926954315; -6.721970042502124e-5 0.00044831034406358453 -0.001138951077275381; 0.000989557326982761 0.000420097644898213 -0.0006913040585871419; 0.0002566333864609722 -0.0002749875296690779 -0.0011938250306982553; 0.0005318056111716727 -6.719438268357268e-5 -0.0011189304372628303; -3.366775003612991e-5 0.0007284202866357904 -0.0017591850600389108; 8.538360184565119e-5 -0.00010361173948359459 -0.0005325340568649297; 0.0004636653513718765 0.0003428922462141754 0.00015379844652323548; 7.976485708870439e-5 -0.0005145049735409311 0.00010768004417480886] %
Mass Used: 125.54754001670926 kg
Launch C3: 90.58035609704275 km²/s²
||V∞_in||: 0.0002551832890214541 km/s