Files
thesis/archive/ES_0.6537729994270098
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6537729994270098---------------------------
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: 2024-05-09T05:12:54.064
Launch V∞: [7.691808430109205, -7.622329098574237, -2.760688581939663] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.0014211169010560363, -0.0012806383604121738, 0.0010613219299235816] km/s
V∞_out: [0.0016679766273592128, -0.0011226451762086, -0.0008628765761140208] km/s
time of flight: 9.916704743067868e7 seconds
arrival date: 2027-06-30T23:37:01.064
thrust profile: [0.08128927470371286 -0.04076879394703848 -0.05345836108733848; 0.09130877308728491 -0.0055555513526672545 -0.1032520571616378; 0.08364554197329396 0.01121624450479071 -0.13661682335521835; 0.060401118807653385 0.014596752266695706 -0.12729838487387113; 0.043358012378052375 0.013472958191447108 -0.11055091254271632; 0.02854086536616249 0.010181627672886289 -0.08506478897967164; 0.016724838775710155 0.006521544528584322 -0.05709398039201795; 0.008069624836304764 0.003365764633577214 -0.03128834693571072; 0.003067316573771935 0.00119511020112518 -0.012019817350853518; 0.0004325275674672139 5.9167477278974126e-5 -0.0007983435152326453; -0.0001983789107227377 -3.0584993859840404e-5 -0.00040288830106929537; 0.0003813536469743853 -0.00020353001575637664 -0.0003304287529994269; 0.0006523370240128744 9.548957707135944e-5 -0.0007777949565320147; 0.00010900320532758962 -0.00020539928593174282 0.0006309590254971395; 0.000333682275389908 0.000375159916250417 1.6636806981031526e-5; -7.531133958902099e-5 0.00041393086698232324 -0.00016481300295796204; -2.3719069875272026e-5 -0.00018004047838761947 -0.0005040590082074242; -0.00015931170830172907 8.619666566924127e-5 -0.0006603652179871449; 0.00020449100874368633 0.00016296749624851258 0.0003525204910551781; -0.0001181731200623682 -8.94466536717751e-5 0.0005502860986408089] %
Mass Used: 34.238053654462874 kg
Launch C3: 124.88521925892262 km²/s²
||V∞_in||: 0.0021876956130968054 km/s