Files
thesis/archive/ES_0.5632225216242194
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5632225216242194---------------------------
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: 2023-05-01T23:55:23.394
Launch V∞: [6.105067282789713, -7.594996475895405, 0.1342876250539707] km/s
Phase 1:
Planet: Saturn
V∞_in: [-8.898706683666214e-7, -2.2653589114267853e-7, 2.964879140545136e-7] km/s
V∞_out: [-8.286724323421346e-7, 2.1090139827314727e-7, 4.27222340700214e-7] km/s
time of flight: 1.855517070472798e8 seconds
arrival date: 2029-03-18T14:03:50.394
thrust profile: [0.4266372497212314 -0.08916067645660763 -0.12852740420528397; 0.09111933991137172 0.029564967330773784 -0.08753053237270998; 0.07143348806452875 0.04335669467093039 -0.11362214676717008; 0.06310620160860532 0.053254657170512414 -0.1414538294139545; 0.05383533635906032 0.055606363552739735 -0.15401179623398453; 0.03647040788285928 0.04430616098618881 -0.12714735835000254; 0.017385125609271714 0.023349203114559732 -0.07556217641710854; 0.011687118069162157 0.017313848593892314 -0.05884713235742516; 0.0018475133416284717 0.0028569854642211743 -0.010759796356913395; 0.0036802150884410402 0.006345741572364066 -0.023789498836465063; 0.0015738571230519433 0.0008598231002259985 -0.0009784427979447014; 5.330454046013669e-5 0.0003591064622844192 -0.0010484364922741572; 0.0004975716920907268 0.00025643365383752576 -0.0011046738105854213; 0.0003521420157559356 0.0002392748817144927 -0.00082395361721724; 0.00011015274600700533 0.0005918812594560522 -0.0011591860216217291; 0.00033603260361265877 0.0004851232586332779 -0.00018930568267393644; -1.3854051312562048e-5 0.00020767660565723374 -0.0012728635878778917; -7.736480604994723e-5 -0.00016693979308602218 0.0015151890410880476; -0.0009580257678192658 -0.001701063205821965 -0.0005346648093872933; 0.0019469828933343014 -0.0015952049391673494 0.0005329129480252835] %
Mass Used: 103.07881011369818 kg
Launch C3: 94.97385116249562 km²/s²
||V∞_in||: 9.649318108423318e-7 km/s