23 lines
2.0 KiB
Plaintext
23 lines
2.0 KiB
Plaintext
archive/ES_0.5601053284232422---------------------------
|
|
|
|
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: 2024-05-14T13:05:10.102
|
|
Launch V∞: [7.674714306571231, -6.013734106756503, 0.0056394642611274325] km/s
|
|
Phase 1:
|
|
Planet: Saturn
|
|
V∞_in: [-4.70880398126339e-10, -1.8515658457460911e-9, -1.571101635557064e-9] km/s
|
|
V∞_out: [-3.6793829576568253e-9, 2.852177997942969e-9, 2.0538815259214184e-9] km/s
|
|
time of flight: 1.825937337566871e8 seconds
|
|
arrival date: 2030-02-25T21:34:03.102
|
|
thrust profile: [0.4609587274693095 -0.018621318774157753 -0.12044216231854117; 0.07552515540186583 0.04327235540321104 -0.0878722551782157; 0.06663578703728022 0.06510734211936826 -0.135215559901146; 0.029140431916059445 0.036629062642035665 -0.09102069997022047; 0.019232019091256387 0.029344712700110617 -0.08059813919212434; 0.013394992082066026 0.025068127567770552 -0.07423239105693015; 0.013033408555517836 0.028029427287103607 -0.08095722470180108; 0.005485744718925089 0.013438932214049298 -0.04651177791748746; 0.008206287728904057 0.02325792467811531 -0.08034354361040381; 0.005022393780606013 0.01649966804262205 -0.06357111363487292; 0.0005588912104434608 0.0012174839866099256 -0.004942192966698465; 0.0005385106062652252 0.001421035712640482 -0.0024982068815134267; -0.0004434701869965676 -0.00023931097990737308 -0.0013884104639172844; -0.00014837827108566776 9.441900884675982e-5 -0.003680014903637654; -0.002419802193647462 -0.00342138512964707 -0.003019445537081227; -0.002988554448405345 -0.0002858501123549639 -0.008903375264521937; 0.002559505907388231 -0.0010752933871574044 -0.000642838055845947; -0.0003742117585363294 -0.0008009456145316998 -0.0009012161557354275; 0.002035778667404846 -0.003598633995828141 -0.0032442898431030943; 0.0010029702282087207 -0.002558315004166785 -0.0020627737858351907] %
|
|
|
|
Mass Used: 98.90297833987506 kg
|
|
Launch C3: 95.06626939781272 km²/s²
|
|
||V∞_in||: 2.473536896778202e-9 km/s
|