23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5596322486099483---------------------------
|
|
|
|
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: 2024-05-15T02:41:29.580
|
|
Launch V∞: [8.025154703949166, -5.883671004882501, 0.21657321369510946] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.400227544820904e-7, -1.1028448617171174e-6, -3.239391762318676e-6] km/s
|
|
V∞_out: [-3.086084062734637e-6, -4.3242092729436743e-7, 1.4192699798234924e-6] km/s
|
|
time of flight: 1.8250280203686887e8 seconds
|
|
arrival date: 2030-02-25T09:54:51.580
|
|
thrust profile: [0.1515874289278483 -0.011907117061099832 -0.057230490608955076; 0.06584179254040708 0.027231028674008097 -0.08483475064207431; 0.03703156400340408 0.023513790421956945 -0.08176939536353917; 0.03077111608863818 0.02399127723354494 -0.09727090406160822; 0.02177688189846801 0.019395729402066655 -0.08837904077346194; 0.03131850037766497 0.030727831918124872 -0.15930931679774066; 0.01937899064540146 0.020662556310211536 -0.11740504578469922; 0.0045341958442245015 0.005735079575105704 -0.02605476028823668; 0.00975958082008779 0.011198943155710033 -0.06814673809196495; 0.00020957638596794202 0.0003908312982174365 -0.001429392989801018; 0.007639570311956006 0.004662740665206025 -0.027729455424914718; 0.0022220264024919245 0.002368955548891453 -0.01742071430268089; 2.2847213808437907e-5 0.00046946214437555293 -0.0028055736855313908; -0.0016661462791229195 -0.0010995691758948515 0.0044427160089068165; 0.0009533756387059697 0.00011074717381194787 -0.0031582610247531213; -0.00016262698650426803 -0.0023863675064505463 -0.0020161954559545455; 0.001541835735202621 -0.002755801938673837 -0.00262611984523634; -0.010345756325464342 0.007652320427818665 0.00043084728881184883; -0.001551457657860445 0.0010154756434123564 0.0012188605482585336; -0.0007798993849617907 -0.0010804790038240007 0.0034995168838565464] %
|
|
|
|
Mass Used: 75.00997728634047 kg
|
|
Launch C3: 99.06759647290272 km²/s²
|
|
||V∞_in||: 3.430384337281045e-6 km/s
|