23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5657591726874239---------------------------
|
|
|
|
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: 2023-05-04T09:13:54.997
|
|
Launch V∞: [6.302201292759959, -7.70139819108994, 0.3064553895008882] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [0.017332843819947184, -0.007155055100200915, 0.018690407608097065] km/s
|
|
V∞_out: [-0.016759292173538175, -0.006676242641393704, -0.019376975123308875] km/s
|
|
time of flight: 1.824529965390573e8 seconds
|
|
arrival date: 2029-02-13T02:37:10.997
|
|
thrust profile: [0.22256450033272593 -0.07967313647567968 -0.09811366168578023; 0.023522653144497706 0.0016814800226277423 -0.03251416296966754; 0.0342235778211872 0.006233451065174104 -0.0798570202906673; 0.039323465999224184 0.009392553022744627 -0.12646980159338786; 0.04003023780607063 0.010381998806152967 -0.15886412803333422; 0.041813349621203345 0.010769219640947672 -0.19635458379639842; 0.02315497642053556 0.00573663232912809 -0.12264574197732393; 0.007116577076780474 0.001649750450100653 -0.04378988595746871; 0.002596475784843862 0.0005440102662051027 -0.01806756916634421; 0.003588147072310581 0.0007382184402246487 -0.025893983348839626; 0.002189415219801784 0.00037954663813766513 -0.01765701658211894; 0.000256879616748989 0.00047864542329736014 -0.004755053436568513; 0.0004078799911084337 -0.00017213437091591468 -0.0026086290041599713; -4.2101976323650895e-5 -0.0006062040564083562 -0.0010523076800088376; 0.00015847862817106983 0.0002398840407134581 -0.0005116145190652178; -0.0007503967869934586 -9.696352406895228e-5 0.00038389978786007085; -0.0001562711922910071 -0.0001301066012068751 0.00010251078973329584; -0.0013913098184539282 5.99922628829371e-5 -6.292075874830957e-5; 8.06134498384865e-5 -4.982175075468663e-5 -0.0014035883113688952; -0.00012065364174817723 -0.0004961848043227872 -0.00016707940086918734] %
|
|
|
|
Mass Used: 81.833758997328 kg
|
|
Launch C3: 99.12319013794284 km²/s²
|
|
||V∞_in||: 0.026475528794160187 km/s
|