23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5844830460863794---------------------------
|
|
|
|
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: 2023-04-20T22:47:59.844
|
|
Launch V∞: [5.2767534041607815, -8.095152340143207, -0.45186443495622886] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.7929109094608683e-7, -2.7914489648318414e-8, 3.782083831383665e-8] km/s
|
|
V∞_out: [-1.8403229429222557e-7, 1.7249874111949938e-8, -2.2571353803000036e-8] km/s
|
|
time of flight: 1.4011999537279135e8 seconds
|
|
arrival date: 2027-09-28T17:01:14.844
|
|
thrust profile: [0.6741756666453782 -0.39463395127346024 -0.2716915486330256; 0.2683487100630184 -0.006237592730915228 -0.2570043397660399; 0.13752507780855314 0.028111767108811216 -0.20619370229935066; 0.10888637248947705 0.03773075136673941 -0.21477802509008145; 0.0654520127074445 0.028889969248889258 -0.15912407175060336; 0.058078791033772496 0.029512513897478044 -0.1627199235406265; 0.07102405119603483 0.04173696852180939 -0.21753889564319773; 0.02148951293592413 0.013606271485094152 -0.07893285953988599; 0.005847859502882349 0.003555850449047893 -0.019503771065999754; 0.006229516826065072 0.005130681295128397 -0.028306940194158366; 0.0037860171954020336 0.00020712611955330537 -0.009120478380784964; -0.0008921308380056656 0.0001553283504622663 -0.0006336661649505066; 0.00024655676890692987 0.0005070038226954615 -0.0006568211853918149; -0.00016368919830580988 -0.0003408306853624329 0.0003779264389616962; -0.0008681984070967464 -0.0007041858974755409 0.0016282996480864547; -0.00040463504975488574 0.0026532880631572574 0.004270581759814751; -0.00034444180239051093 -0.0005855196326192767 -0.0017474104756779242; 0.0010414695286879814 -0.0038127484449128847 -0.000527138640506626; 0.0002452126705276565 0.0008568318450092403 -0.0005274036540408554; -0.001742965597880856 -0.0024024392668315726 0.002983005495902543] %
|
|
|
|
Mass Used: 136.01472413228657 kg
|
|
Launch C3: 93.57979936602675 km²/s²
|
|
||V∞_in||: 1.8535082906673343e-7 km/s
|