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thesis/archive/ES_1.148469222320979
2022-04-18 10:59:25 -06:00

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archive/ES_1.148469222320979---------------------------
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: 2023-01-18T05:47:39.532
Launch V∞: [-4.417549910925255, -5.897163172582938, 0.3311367280281343] km/s
Phase 1:
Planet: Saturn
V∞_in: [0.004020236426475727, 0.00011823227234776388, -0.0027387450871508077] km/s
V∞_out: [0.004711851444026571, -4.628123695743769e-5, -0.0013497561988335854] km/s
time of flight: 1.8390221785801837e8 seconds
arrival date: 2028-11-15T17:44:36.532
thrust profile: [0.05014064318073163 -1.0 0.011461045655650651; 1.0 -1.0 -0.05951953393497983; 1.0 -0.6375447540282521 -0.08586812521824527; 1.0 -0.0363232956336098 -0.08649535523559387; 1.0 0.3344854524769929 -0.09694329338209909; 1.0 0.6243665041315285 -0.10749063430948069; 1.0 0.805126616436485 -0.11035145902657019; 1.0 0.8933710053774171 -0.10638128005702555; 1.0 0.9145066889017774 -0.09817654691499737; 0.9878134500090321 0.8746780543751003 -0.08623176020672403; 0.7753482143833724 0.7457849743190975 -0.06861092830597851; 0.4547913770694951 0.4782291218561762 -0.042160998501724854; 0.030812702576755592 0.03489021821430756 -0.003234716161380927; 0.0007243532730815151 0.0009397060291191669 -6.758005439942867e-5; -0.0005471889385547713 0.0018621983636613545 0.00022874404932698338; -0.00040197724227040716 -0.0003774740000732099 -0.0005178131097494307; -0.0005073724647809426 -0.0013085143770457022 0.0025048616188134386; -0.0014692750736326552 -0.00046767523696134657 -0.00038106568258965026; -0.0003348029999094244 0.0008718645566854262 0.00013545927908464774; 0.000721953677793413 0.0006850819594771289 3.1347672637998146e-5] %
Mass Used: 1022.5419880197805 kg
Launch C3: 54.40093223223338 km²/s²
||V∞_in||: 0.004865902223368194 km/s