Files
thesis/archive/ES_0.5641700386408275
2022-04-18 10:59:25 -06:00

23 lines
2.0 KiB
Plaintext

archive/ES_0.5641700386408275---------------------------
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: 2024-05-08T21:44:36.848
Launch V∞: [7.602188440161492, -5.657857419288432, 0.2510955435696445] km/s
Phase 1:
Planet: Saturn
V∞_in: [1.1290863926579886e-6, -3.8783416275469056e-6, -1.1155635979019294e-5] km/s
V∞_out: [-1.086720593654847e-5, -1.2887779482476677e-6, 4.571043268032056e-6] km/s
time of flight: 1.8444305195201132e8 seconds
arrival date: 2030-03-13T15:55:27.848
thrust profile: [0.8431128004942959 0.0003420768372455901 -0.16472850832853925; 0.15011106656260145 0.10205785759501312 -0.11979985841045818; 0.0534750718332628 0.06249009216521422 -0.08472949983292394; 0.02967985800502251 0.04772509416290628 -0.07554491018967904; 0.05381382948824906 0.11470478757640389 -0.17783995620807638; 0.011791665310708337 0.030434667250716554 -0.055061385413384165; 0.0071964464908520825 0.03140947219203327 -0.05929106543686528; 0.0027408964414759257 0.007993991230665186 -0.018629239412255326; 0.0013611753491884987 0.012423457351484875 -0.026496468583554793; 0.0027341955976295023 0.016522429785322864 -0.035912770070806295; 0.0037599287548372626 0.024490756287742204 -0.05240251955109946; -0.002392448161233306 0.00024356751524128029 -0.0008657029636573799; 0.0017637512389544212 -0.000550755570869236 -0.004371317454262478; 0.0029823239028410184 0.002720032926583411 -0.0015125258571859037; 9.979084609980214e-5 -0.0001816940115874936 -0.001793329111761833; -0.0025699720104042506 -0.0051101442915238915 -0.0026067110156898807; 0.0005285389655088438 0.003159366663157502 0.0013330865559545105; -2.9675193924589843e-5 -0.00020404953675948092 0.0008667993532017583; -0.002940923921874053 0.008111282379992216 -0.002729974967538732; -0.0038538529782692474 0.0019452687075129683 -0.0025997773834439135] %
Mass Used: 133.9703114134163 kg
Launch C3: 89.86766862872271 km²/s²
||V∞_in||: 1.1864425142350488e-5 km/s