Files
thesis/archive/ES_0.6343539548119961
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.6343539548119961---------------------------
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: 2024-04-21T14:45:25.277
Launch V∞: [7.473211938294323, -5.685438185128409, -0.32406262021073373] km/s
Phase 1:
Planet: Saturn
V∞_in: [-9.769996985674197e-10, -5.4705918706626785e-9, -4.143214439696908e-9] km/s
V∞_out: [-1.5266667452511553e-9, 1.5127194755349298e-9, 1.2484231321208659e-9] km/s
time of flight: 1.8101255168232054e8 seconds
arrival date: 2030-01-15T16:01:16.277
thrust profile: [1.0 -0.10264633793817766 -0.12740764769992335; 0.6918965496933761 0.42470739092159443 -0.28653552145914535; 0.3593069207599869 0.4013518705213481 -0.2732146366805213; 0.15835522823664178 0.2550446440473887 -0.18804281990285315; 0.08503004474900652 0.18276346107708907 -0.14498545889435094; 0.006505927211677154 0.018068558379632862 -0.01714579395361096; 0.0012468862247601252 0.004280923514716375 -0.004121702395254169; 0.00036588365392897223 0.0015539328071533525 -0.0016011069877575885; 0.0001278365905605107 0.0006757683197418397 -0.0006903282252369992; 0.0005820306084223725 0.000910363737282687 -0.0005965637824065265; 1.722670133222305e-6 0.0008748576558242809 -0.0011467404601399256; 5.0422382627007145e-5 0.0005546543301036709 -0.0006060530305168968; 0.00014701767567332598 9.523608962610478e-5 -3.063881264012944e-5; 0.00014506836424228161 0.0006549028737236953 -8.1035871039502e-5; -8.925899952378285e-5 0.000396883953839062 -0.00048676249230035474; -1.597810726424939e-5 -8.080612839739883e-5 0.00012655964777649758; -0.0002792463833492289 0.00015548816574584284 -1.913883537920047e-5; 0.0005898169927245843 -0.0006964523317549166 -0.00020975820394034025; 6.466602016552949e-5 0.000518554282547793 -0.0003908409958206972; -0.0002235136903379966 0.00042771184996658203 1.417471725169157e-6] %
Mass Used: 225.1239103691687 kg
Launch C3: 88.27812061339885 km²/s²
||V∞_in||: 6.931675823325437e-9 km/s