23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5696699681842783---------------------------
|
|
|
|
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: 2024-05-07T02:22:18.831
|
|
Launch V∞: [7.458160009670592, -5.773267087205727, -0.5121477903828789] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [2.3093786551735795e-6, 2.332671704245062e-5, -0.00045150519920282464] km/s
|
|
V∞_out: [-1.8930062760453904e-5, 0.00045249555676124683, -4.854555394363561e-6] km/s
|
|
time of flight: 1.815031821594033e8 seconds
|
|
arrival date: 2030-02-05T19:55:20.831
|
|
thrust profile: [0.7687271939859782 -0.01870773194972288 -0.1773694461744846; 0.3161378497769775 0.1986596928124878 -0.2360587567218027; 0.1260087567534983 0.13867542355682833 -0.18087607109565929; 0.0234237956464292 0.03682746257343391 -0.05928365122233981; 0.02128592416779429 0.04376215668272925 -0.07468782784794781; 0.020600271515052643 0.05078564819609578 -0.09206091769148897; 0.01357300550802619 0.045409283260505084 -0.08561118700424956; 0.0011192417796989916 0.010425243861678623 -0.020686527907026752; 0.0007093565156696245 0.002871126232388356 -0.009215148457185168; 0.0038015845189509566 0.03137915198641237 -0.06757710038310509; -3.9126675089101053e-5 0.0005402031259571511 -0.0016813277449456774; 0.000690516428042157 0.00018373664362874567 0.0016135729643282186; 0.0002349851598580907 0.00036452000519434074 -0.0027498269446664114; -0.0028545706394788213 0.000796311731855955 -0.002175180813627303; 0.0027955716307904157 -0.0032022279878911085 -0.00036677262033965607; 0.0025326585583373045 0.0023955632057973504 0.0007599489153483751; -0.0033174738840312454 0.0028817663116878904 -0.0004930143020850759; 0.0011294375529773285 -0.00040839313981149957 -0.0016005311564528998; -0.0009580057753038112 -0.0014775494807219305 -0.0026197403744932274; -0.00020837098146317477 0.0008767554917773631 0.0004753442059071627] %
|
|
|
|
Mass Used: 144.18211901099448 kg
|
|
Launch C3: 89.2170589492566 km²/s²
|
|
||V∞_in||: 0.0004521132754796456 km/s
|