Files
thesis/archive/ES_0.5600152936704055
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5600152936704055---------------------------
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: 2024-05-10T15:20:23.119
Launch V∞: [7.956732759833716, -5.582668797787937, 0.1898722211164827] km/s
Phase 1:
Planet: Saturn
V∞_in: [-1.6404902831304344e-9, -7.786738976715708e-11, -5.682680582146815e-10] km/s
V∞_out: [9.76805179062555e-10, -7.139096496153755e-10, -5.93870478067325e-10] km/s
time of flight: 1.8749577787471613e8 seconds
arrival date: 2030-04-19T17:30:00.119
thrust profile: [0.4046349609505755 0.01905847768378913 -0.09651277475646815; 0.15774731110147558 0.11274980470654986 -0.1354628377212629; 0.067120306892142 0.08070627876854986 -0.11174034246212965; 0.054334514579795615 0.09101037977643722 -0.13692486653330577; 0.036802124910846536 0.08016707773363897 -0.1323999848796748; 0.010728513328168059 0.030763878029976124 -0.059132981023344855; 0.007852706010007565 0.02989037267087798 -0.058793088589345226; 0.0047833270087636265 0.019647762806647765 -0.044722633750739926; 0.0025097555859229853 0.011649203831070775 -0.02509125519060137; 9.810714885539143e-5 0.00021197715888701836 -0.0013260872417469186; 9.695363033138217e-5 4.708698866122602e-6 6.747331460415585e-5; 0.00016364517052377045 0.00014635494913496427 0.00029165710210131445; -0.00020841135175774775 -0.0007150467002401085 -0.0005531551858579472; -5.4819110324114595e-5 0.0006799585543226308 -0.0014583744634044306; 0.001160777686659555 -0.000974817112103091 0.0006537003418269156; -0.0007984034990295971 0.0007798871556691706 0.0016131919940809468; -0.0004258032119940583 -0.0017078044778460705 -0.0004748922867346216; -0.00027135797846957463 0.000635116825881635 -0.00016309196048702387; -0.0012474297044015679 -0.000644132967680312 0.002793529145154105; -0.002830292906502924 0.0012045899668355507 0.002039142570176561] %
Mass Used: 102.0321175797194 kg
Launch C3: 94.51183857755777 km²/s²
||V∞_in||: 1.7378723443974842e-9 km/s