Files
thesis/archive/ES_0.5667306448152907
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5667306448152907---------------------------
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: 2023-04-29T20:39:16.393
Launch V∞: [6.745076355016234, -7.291736982592519, -0.7894087430014743] km/s
Phase 1:
Planet: Saturn
V∞_in: [-6.814862267093487e-7, -0.0002253786986265147, 0.00015265804438600552] km/s
V∞_out: [0.00012635246918063422, 0.0002356196513918851, -5.155965208602473e-5] km/s
time of flight: 1.8599753299570274e8 seconds
arrival date: 2029-03-21T14:38:08.393
thrust profile: [0.14845518860429355 -0.04274468347592668 -0.059443223292437425; 0.06715705768454897 0.016473162663041288 -0.07881873989156553; 0.05978047827818915 0.029647905541643135 -0.11913873171544906; 0.05061815415176844 0.034083235365301265 -0.14265355379089836; 0.039320195895561925 0.03215320241836776 -0.14317848362803623; 0.02958432289198864 0.027901728874934015 -0.1319785763313595; 0.020442473854680735 0.02158558277283701 -0.1078339168108192; 0.0121628795503699 0.014128775239653822 -0.07416613212962966; 0.004792172964557708 0.006106959926069187 -0.03396425856220845; 0.0011241151846404659 0.0014203166173432388 -0.009934465219481636; 0.0007100199867284691 0.00034054416554506396 -0.0023915034800194705; 0.0003542382319391105 0.0003979271725010715 -0.002355588659943224; 0.00045755323186733444 0.0006017542145975597 -0.004112578731449028; 7.876094596899043e-5 0.00029132245010692927 -0.0017511531586588572; -0.0012874737117114087 0.0006773854600605214 0.00038689067302674434; -0.00018001487258012002 0.00010082555101252735 -0.001292852085103302; -0.0015954917214033922 7.693922965036046e-6 -0.0023700984948638896; 0.0006891478859853109 -0.0002781406005922935 0.00113813906671592; 0.0017300336640872415 0.0008257526608876811 0.0001325540203784014; 0.0003847498374599611 -0.00023228255343627966 0.0019225669785602586] %
Mass Used: 82.00196399047582 kg
Launch C3: 99.28864942183371 km²/s²
||V∞_in||: 0.00027221407152059235 km/s