Files
thesis/archive/ES_0.5587199593773109
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5587199593773109---------------------------
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: 2024-05-14T01:41:30.416
Launch V∞: [7.565812903949794, -5.940407824187746, 0.028617729545849024] km/s
Phase 1:
Planet: Saturn
V∞_in: [-0.00024412979782694865, -0.00019875332121081622, -0.00016578847083511625] km/s
V∞_out: [-3.534383916194474e-5, 0.0002217976487915621, -0.00027507763847841986] km/s
time of flight: 1.8540233206889987e8 seconds
arrival date: 2030-03-29T22:20:22.416
thrust profile: [0.5982177269354307 0.0056748187022684065 -0.16845604326454242; 0.1664312374095709 0.10002404501515162 -0.17006830888883964; 0.05278958320979118 0.051286386808336935 -0.10276507146864626; 0.04710138501306585 0.06169184924025577 -0.1360143015309248; 0.031718714944501535 0.051582254318170276 -0.12588729436503826; 0.012033906654512622 0.02332164968328359 -0.06409683435800292; 0.009119256836362296 0.020058575990145575 -0.0577459769922098; 0.004128087139752802 0.01151245887139821 -0.034284087828072296; 0.00043847439526424836 0.0016876510579877852 -0.006054983543550661; 0.0012065281453279837 0.0010519907043614913 -0.0024741137662263176; 0.0003112402943840093 0.001126265301584001 -0.002864593064564292; -0.0015569023392716845 -0.001608131868653303 -0.0038980875070938103; 0.0008633367958258623 0.002585776255155346 -0.0004396483308994484; 0.001624434194870437 0.000131294362031019 -0.004041891223628885; -0.0020657763012795743 0.001109715936295498 -0.0027008019806173773; 0.00017491161687749356 0.0011510498592219019 -0.004826022853802063; 0.002771714695851585 0.004888745178745769 -0.004675122731148756; 0.0001533439022232077 -0.002061321526192954 -0.002461900941259724; 0.0006476747056970188 0.0007276711892223941 0.0027265400623846937; 0.0016846208646642091 -5.850225933004037e-5 -0.001732647401004721] %
Mass Used: 112.07701683367941 kg
Launch C3: 92.53078898968856 km²/s²
||V∞_in||: 0.0003557921555363509 km/s