23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5631403985984627---------------------------
|
|
|
|
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: 2023-05-02T13:38:21.158
|
|
Launch V∞: [6.4226731963173425, -7.678284206159425, -0.05474095354976099] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-0.011859103011865026, -0.0003662021147496042, 0.008856882889335477] km/s
|
|
V∞_out: [-0.01419833870586378, 0.00013883325423149503, 0.004193473263725734] km/s
|
|
time of flight: 1.809203485145635e8 seconds
|
|
arrival date: 2029-01-24T13:17:29.158
|
|
thrust profile: [0.061570234559453804 -0.020356331311062296 -0.027394317265341514; 0.03965466085304665 0.005812214432066018 -0.05144151863742983; 0.0386770221972752 0.013090259959421048 -0.08303240082487709; 0.06000265925098331 0.027649546987385695 -0.17240475863759366; 0.049581968832447115 0.026913520318714967 -0.18023638091250732; 0.026731575520830633 0.01589831944706889 -0.11981872497684545; 0.024261410038258217 0.015856202168346132 -0.1260274737926133; 0.008656559691985276 0.006258112777299956 -0.0533058948820863; 0.00948055720103211 0.006678075567504091 -0.06259990121771841; 0.0012808956290852164 0.0010409196089788775 -0.010106175027331486; 0.0020527026045108216 0.00102108482092573 -0.018323217493909787; 3.1601663024984766e-5 3.502272103345761e-5 -0.00030105264201264027; 6.4073760135454e-5 0.0001255819530441597 -0.00044537352025355475; -3.0444290775113482e-5 4.321157134829488e-5 -0.0003326486899640284; 2.169741404204757e-5 0.00010098533616124868 -0.0002695816578859818; 0.00019437090721700911 8.289205636891062e-7 -0.0001255168192746938; 0.0003767522729381086 0.0004133121665881494 6.455905014356037e-6; 0.00011542348054990978 -0.00016189227960509322 -0.00012841141688303004; -0.0003350414220344559 0.0001664469573420226 0.00013545112257822337; -6.721839988223824e-5 0.00042710027347691123 0.0011730215298246353] %
|
|
|
|
Mass Used: 72.44010556093781 kg
|
|
Launch C3: 100.20977590924605 km²/s²
|
|
||V∞_in||: 0.014805971861052442 km/s
|