Files
thesis/archive/ES_0.6460746953916008
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6460746953916008---------------------------
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: 2024-05-08T08:53:45.607
Launch V∞: [7.443623830532165, -7.51627542986256, -2.461546034022452] km/s
Phase 1:
Planet: Saturn
V∞_in: [6.806869714498327e-5, -0.000838622425167826, 0.00011424888376010094] km/s
V∞_out: [0.00025485782081825255, 0.0005440652258631785, 0.0006000364057680866] km/s
time of flight: 1.0067906880750838e8 seconds
arrival date: 2027-07-17T15:18:13.607
thrust profile: [0.5029233713364502 -0.25928308888025153 -0.29416720403769986; 0.21173537217391097 -0.016480730817907442 -0.23038687657656312; 0.11068793113273556 0.011835417357807425 -0.18140992577368775; 0.08952598112974788 0.01861582556904238 -0.18986354724896606; 0.044200255935823586 0.012492044065448222 -0.11377166904753722; 0.014165606807611697 0.004661229333521733 -0.04030353322889887; 0.007244378353125538 0.001264477770383152 -0.023091758273428742; 0.008714504872061336 0.0042567621030144285 -0.03522462785133937; 0.0017898080824324213 0.000831459613085983 -0.007169701765191981; 0.006672918786073544 0.0044789398334471545 -0.017705537235030443; 0.00014902253331400083 0.00032168107577215264 -0.0002982733280600607; 0.0001462065856855511 0.0009624628464273416 -6.578849739105911e-5; -2.7992668619460537e-5 8.317145931858216e-5 -0.0010491924412001836; 0.0008449490860829745 -0.0004569289431436775 -4.708349893925781e-5; 0.00014107203935206868 -0.0010555227051595765 -0.00016877015121456024; -0.00013597657334394418 -0.001107908165665271 0.0001643315599519689; -0.0004095359021096171 -0.00018065668367957705 -0.0005910626139062891; -0.00038420488009707266 -0.0004362676796358821 -0.00047783448354832595; -0.000499082159185766 0.0008740852801460272 -0.0008551571227561302; -0.00035677773753636327 0.0007571750467310789 0.000684846474369777] %
Mass Used: 65.64715577400466 kg
Launch C3: 117.96114094563363 km²/s²
||V∞_in||: 0.000849101717679225 km/s