23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5839476374569075---------------------------
|
|
|
|
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: 2024-05-07T07:42:51.235
|
|
Launch V∞: [7.128935389342506, -6.924375611272405, -0.849081287728507] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.0443306122642861e-5, 2.8247005572891275e-5, 1.4287114860109724e-5] km/s
|
|
V∞_out: [2.459025441824638e-5, -1.8881205909940463e-5, -1.2241464675870153e-5] km/s
|
|
time of flight: 1.4136376334740674e8 seconds
|
|
arrival date: 2028-10-29T11:25:34.235
|
|
thrust profile: [0.2608132744824838 -0.09006249543038877 -0.12016725302991846; 0.1487014973411549 0.01934963331464867 -0.17292431732219865; 0.095075559613888 0.03196814940247515 -0.18027844047633879; 0.06698913102501199 0.031014786419621965 -0.17229145422558015; 0.06197597663315511 0.033745406217724705 -0.20099347145359592; 0.05530172949233382 0.03339459394368057 -0.21143818030637926; 0.022709575857232663 0.01611144042206957 -0.09895733490818562; 0.028466270432626728 0.019886830669683827 -0.13750754487629963; 0.006368421667849616 0.007038601416022496 -0.04474295088851109; -0.0022032432865858645 0.00630614947056097 -0.010890519694786807; 0.0054666167660472895 -0.0021364664428610665 -0.0063459924548353265; 0.004082041753076653 0.003030947493904761 -0.02271407407462264; 0.006740819635405076 -0.00705093972349292 2.0169009807825128e-5; -0.0034371066954555322 -0.004563549015335934 -0.004566103611076908; -0.001781028272794643 0.0040415649445208635 -0.000419219205844484; -0.003945922949769072 -0.0041189794347444905 -0.004564859172828619; 0.012547786417152176 -0.008225421708726735 -0.0017835594348521132; 0.01259562165522743 0.004851752515968906 0.004648290205531096; 0.016295140670391492 0.015234798834997863 0.000986496686562122; -0.012622940124363432 0.01472063337129927 -0.002189856221886846] %
|
|
|
|
Mass Used: 100.91603122303923 kg
|
|
Launch C3: 99.48963642457477 km²/s²
|
|
||V∞_in||: 3.333283092736272e-5 km/s
|