Pollux Castor – Simulation results
Engine selection
[J400-*] [J350-16 -5 ]
Simulation control parameters
Resolution: 800 samples / second.
Simulation method: Explicit Euler.
Simulation execution time: 13.525 Sec.
Launch conditions
Altitude: 0.000 m
Relative humidity: 50.000 %
Temperature: 15.000 Deg. C
Pressure: 2.493 Ft. Hg.
Wind speed model: Calm (0-2 MPH)
Wind turbulence: Fairly constant speed (0.01)
Wind starts at altitude: 0.000 m
Launch guide angle: 0.000 Degrees from vertical
Latitude: 1.571 Degrees
Launch guide data:
Launch guide length: 914.400 mm
Velocity at launch guide departure: 24.481 m/s
The launch guide was cleared at : 0.341 Seconds
User specified minimum velocity for stable flight: 13.411 m/s
Minimum velocity for stable flight reached at: 1108.915 mm
Max data values:
Maximum acceleration: Vert: 162.489 m/s/s , Horz: 0.053 m/s/s , Magnitude: 162.489 m/s/s
Maximum velocity: Vert: 312.001 m/s , Horz: 0.894 m/s , Magnitude: 312.001 m/s
Maximum range from launch site: 480.776 m
Maximum altitude: 2736.905 m
Engine ejection charge data:
Conditions at engine ejection charge:
Using a delay time of : 0.000 Seconds
Velocity: 0.000 m/s
Altitude: 0.000 m
Recovery system data
P: Spadochron glowny Deployed at : 24.892 Seconds
Velocity at deployment: 0.283 m/s
Altitude at deployment: 2736.902 m
Range at deployment: -2.388 m
S: Streamer Deployed at : 24.892 Seconds
Velocity at deployment: 0.283 m/s
Altitude at deployment: 2736.902 m
Range at deployment: -2.388 m
P: Pilot Deployed at : 24.892 Seconds
Velocity at deployment: 0.283 m/s
Altitude at deployment: 2736.902 m
Range at deployment: -2.388 m
Time data
Time to burnout: 8.892 Sec.
Time to apogee: 24.920 Sec.
Optimal ejection delay: 16.027 Sec.
Landing data
Successful landing
Time to landing: 474.449 Sec.
Range at landing: 480.776
Velocity at landing: Vert: -5.708 m/s , Horz: 0.567 m/s , Magnitude: 5.736 m/s