23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5657881045423062---------------------------
|
|
|
|
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: 2023-04-29T17:12:15.111
|
|
Launch V∞: [6.048258856363886, -7.756542290659954, 0.15012521686378968] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.025669070522916743, -0.011802133286305238, 0.028547616953914803] km/s
|
|
V∞_out: [-0.027309757536771916, -0.011202456462101528, -0.027232801473037783] km/s
|
|
time of flight: 1.741481366863581e8 seconds
|
|
arrival date: 2028-11-04T07:41:11.111
|
|
thrust profile: [0.2868031962948561 -0.10432240839345934 -0.11217487287296603; 0.1047072456872412 0.015236624864459715 -0.12036864245724832; 0.05339483416925077 0.01895984103255241 -0.10058136955035922; 0.06652288250848734 0.03178531391536626 -0.17029842435632306; 0.05430326624106219 0.03126425151151387 -0.1745796613763504; 0.025079747757995815 0.015282476886909948 -0.09799422052929953; 0.024429347630452427 0.01705547404063272 -0.11080565099187599; 0.015016731806623 0.013307797608910748 -0.08691872509596178; 0.007559208882212915 0.005452232523035572 -0.04551755010243607; 0.0023599508013587072 0.0011229250841690891 -0.011985290939158219; 0.0015298430188493764 -8.062704599568957e-5 -0.0032645220930020017; 0.0017383932723882653 0.0018645940088869882 -0.00894076712696747; -0.0001367523180193884 0.0002739123876739814 -0.004415406224580393; 0.0013620881642410878 -0.001045339908239333 -0.004546124748291904; 0.001283544505590283 0.0007760521935313842 -0.003667913513086194; 0.0004188891064480535 -0.0002041463338012516 0.0003997096827698468; -5.880689832905861e-5 -0.00028912327715629755 0.0009609419803986866; -0.0019128543411607182 0.0037103913260191613 0.0014491546524890778; -0.0007742019199822752 -0.0011869219068879249 -0.001764048544039806; 0.006794413253455122 -0.0022874817114728074 -0.0017732954410963526] %
|
|
|
|
Mass Used: 95.60658232616333 kg
|
|
Launch C3: 96.76792108111896 km²/s²
|
|
||V∞_in||: 0.040164137801845454 km/s
|