23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5645463228022704---------------------------
|
|
|
|
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: 2023-04-30T11:13:50.829
|
|
Launch V∞: [6.019836410215823, -7.62645822561329, -0.2309868665890301] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-1.7129546619263522e-7, 9.621617218942034e-8, 1.5155364937577318e-7] km/s
|
|
V∞_out: [-7.432180534360557e-8, 1.125340698241614e-7, -1.9637061992201233e-7] km/s
|
|
time of flight: 1.806492765875905e8 seconds
|
|
arrival date: 2029-01-19T07:35:06.829
|
|
thrust profile: [0.4504428491471518 -0.1269763175059584 -0.13102760828377466; 0.13691756868270236 0.03749404186614058 -0.14587381320928777; 0.08857094072391614 0.05079483644224842 -0.1603808968230119; 0.03074520883127818 0.020863925656447978 -0.07702082057656726; 0.025653909085989027 0.02136525046159973 -0.08189702579780549; 0.044829315401188334 0.04545510664329023 -0.1768061617391734; 0.02123731780295903 0.023881852133654975 -0.10317901662128975; 0.010509870279037645 0.012367876589150041 -0.05705170427446573; 0.007564814847663893 0.009902505636644143 -0.04698687471968946; 0.002126017039422351 0.002868684201312907 -0.013729389406246266; 0.00209065971012748 0.0009244153486148536 -0.006148256968538561; 7.867555995947706e-5 -0.00012994277601582855 -0.00045893128211693733; 5.670112457590386e-5 0.00010632202676406032 -0.0005120965900366854; -0.00019098824997415553 0.0006187728377167673 -0.0014860714234844036; 0.0006399078736318445 0.0009253086277652559 -0.0004908057823211127; 0.0014368893228703626 -0.0008795135846685416 -0.0015699661410601168; -0.0023889920284884633 0.0005672711960132469 -0.0004270761990573381; -0.0023302338674492822 -7.587954424129515e-5 -0.00011319889539127036; -0.0002674023316661403 0.0023330891220925193 0.0014150903912995222; -0.0010721008149973308 0.0009581702438624877 0.004312436383034456] %
|
|
|
|
Mass Used: 107.65191590494078 kg
|
|
Launch C3: 94.45465040532136 km²/s²
|
|
||V∞_in||: 2.4812939601758437e-7 km/s
|