Files
thesis/archive/ES_0.5573091509392426
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5573091509392426---------------------------
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: 2024-05-12T23:28:25.067
Launch V∞: [7.916412515585392, -5.8577989225252995, 0.03724636466793853] km/s
Phase 1:
Planet: Saturn
V∞_in: [-4.787964580379473e-9, -1.2556514131145832e-8, -2.1427407056275698e-11] km/s
V∞_out: [-2.9453265611491104e-9, -5.97253506047358e-9, -1.5306608326111366e-10] km/s
time of flight: 1.8106874961507207e8 seconds
arrival date: 2030-02-06T16:20:54.067
thrust profile: [0.29820937982735907 -0.01396662803673338 -0.10006639454521657; 0.06945737187937066 0.03514829608967404 -0.08198229086337855; 0.03486647255211833 0.0285232808291748 -0.07378074916440801; 0.03316033162427442 0.03511036679487984 -0.10097495558205016; 0.0375687667515126 0.04823229806672234 -0.149720922159862; 0.023342092722386607 0.03493385549213456 -0.11926823506956541; 0.016857617296177102 0.02833593336503038 -0.10435588013914154; 0.012565789391044841 0.023406337256055346 -0.09204318933387644; 0.0033038831338398997 0.0068133202768387935 -0.029270322737778454; 0.0007419403174370888 0.0017955961060508107 -0.007772891202787391; -1.038598364781014e-5 0.00030296737527921175 -0.0008355037661357166; 0.0004729419550992722 0.0006854661418761272 -0.0015866136287662359; 0.00023218880710936546 -6.109152441084742e-5 -0.0001354469905438336; 0.001643617889495059 -0.0004903160135242015 -0.0010700157119676026; -0.0008943086757368594 -0.0015276220947850541 -0.0002516992665594622; 0.0005769434100349571 0.0006254830607950695 0.0008352741873583651; 0.0007257222455211127 -0.0010870082827923889 0.0005884492575102625; 0.0004034516362799865 -0.0018409318100294418 -0.0001428224611903765; 0.00029116309530394176 0.0009414777616965261 0.0003793456590663158; 0.0002690141196937133 0.0004889769607451331 -0.0008258938598726623] %
Mass Used: 84.44944411465303 kg
Launch C3: 96.98478262533658 km²/s²
||V∞_in||: 1.343841921813747e-8 km/s