23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5667457418720422---------------------------
|
|
|
|
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: 2024-05-07T10:55:23.812
|
|
Launch V∞: [7.7066023889382285, -5.548603990402533, 0.4970704930035837] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.0007016699652531714, -0.0003920300757615782, -2.8991275485303447e-5] km/s
|
|
V∞_out: [0.0005626014377459448, 0.0003514678152391739, -0.0004572164870245832] km/s
|
|
time of flight: 1.8749577785237885e8 seconds
|
|
arrival date: 2030-04-16T13:05:00.812
|
|
thrust profile: [0.6983217584685897 0.016559120228798584 -0.11711740972460617; 0.3159367622350063 0.22434909976097595 -0.19065088234015837; 0.0602298412549247 0.07772609236559504 -0.08273037049039848; 0.029892463280308024 0.055590187228787294 -0.06563294435195706; 0.02033388998540353 0.04809425859811529 -0.06389096121389402; 0.019595474426103324 0.07694123202517826 -0.09911257543165705; 0.012720711895706402 0.07800791117750365 -0.10621872843960622; 0.003525951956268891 0.02268978351964122 -0.03567494197646456; 0.0021414794247714324 0.0169196047255328 -0.028140326350788843; 0.0005423658336329164 0.004622640205010719 -0.007946624949495797; 7.900805526088497e-5 0.0006612241152079009 -0.0010918819824305432; -2.708672894409438e-6 0.0001082358557673946 -0.00019411623740741706; -0.0004265453826960899 0.000372750488103737 0.00038080993952794353; -9.902449812972526e-5 0.00017767928786798564 -0.00021423503719586868; -0.00015776191121870923 -5.3990213334483085e-5 -0.00010409459836805169; 2.541331222425871e-5 1.6923917709060945e-5 -0.00012987034498813493; -0.0006635293177344327 -0.00021416442793834142 9.82212425276814e-5; -0.00029330901215016505 -0.0001895075700679628 -0.0005299616298707708; -0.00020882152253698467 -9.609730350746575e-5 1.8030856861663426e-5; -9.880217472997118e-5 -0.0005008970661738593 0.00023363808356686506] %
|
|
|
|
Mass Used: 133.71949894271665 kg
|
|
Launch C3: 90.42580569851415 km²/s²
|
|
||V∞_in||: 0.0008042815517555281 km/s
|