23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5649117966004618---------------------------
|
|
|
|
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: 2023-04-29T12:24:32.674
|
|
Launch V∞: [6.440088419235104, -7.278942833116861, 0.15878594597612886] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.012641215096916297, -0.00597483158543557, 0.014421297362238274] km/s
|
|
V∞_out: [-0.012812200410408666, -0.005197272924796808, -0.014566103978690445] km/s
|
|
time of flight: 1.8749577787394193e8 seconds
|
|
arrival date: 2029-04-07T14:34:09.674
|
|
thrust profile: [0.47072529767895144 -0.10480402538961694 -0.14469503316804574; 0.09503370213204511 0.031192309275184998 -0.0954786508681824; 0.07698542797629895 0.047797762971574016 -0.12923884395599908; 0.05024686697699967 0.04177205588842523 -0.11983423705427557; 0.03272821648328199 0.03331281452607519 -0.10191491252775546; 0.01968498253918934 0.02384028469837107 -0.07689929798870715; 0.0184609775224742 0.024729067837422177 -0.08439946847219879; 0.007850534898841216 0.011616958261595332 -0.04313086085691365; 0.013600881124577465 0.020956031656204563 -0.08023288588707737; 0.002698183226379533 0.005026993140073463 -0.01937667255648371; 0.0024969233603088317 0.0048936266025735 -0.02000679254846709; 0.0019631906889856906 0.0028498462945074137 -0.009951076180502626; 0.00045769481141511465 0.00048196470078892454 -1.6939326801482246e-5; -0.0003495571195547961 0.0006815132060001066 -0.003306769056313522; 0.000763472780801099 0.0015186025777407914 -0.0065284686113268806; -0.0004763093428787397 -0.002523484980200408 -0.0017529237576039047; -0.0018340298887775065 -4.411524131168565e-5 -0.001517902213330645; 0.006713517163702306 0.003193750804463185 -0.001770807184304665; 0.007922020736406422 0.00267417247093613 0.00030469322858637593; -0.007092588074300684 -0.0004066369430336715 0.00877301719305917] %
|
|
|
|
Mass Used: 107.91315924726996 kg
|
|
Launch C3: 94.48296059198894 km²/s²
|
|
||V∞_in||: 0.020086631106557506 km/s
|