ARLISS Classic (Kenyon) - Simulation results


Engine selection

[M1419W-None] 


Simulation control parameters

Flight resolution: 800.000000 samples/second 
Descent resolution: 1.000000 samples/second 
Method: Explicit Euler 

End the simulation when the rocket reaches the ground. 


Launch conditions

Altitude: 3500.00001 Ft. 
Relative humidity: 30.000 % 
Temperature: 90.000 Deg. F 
Pressure: 29.9139 In. 
Wind speed model: Light (3-7 MPH)
Low wind speed: 3.0000 MPH 
High wind speed: 7.9000 MPH 
Wind turbulence: Fairly constant speed (0.01)
Frequency: 0.010000 rad/second 
Wind starts at altitude: 3900.00001 Ft. 
Launch guide angle: 0.000 Deg. 
Latitude: 40.000 Degrees 


Launch guide data:

Launch guide length: 96.0000 In. 
Velocity at launch guide departure: 47.3976 ft/s 
The launch guide was cleared at : 0.390 Seconds 
User specified minimum velocity for stable flight: 43.9993 ft/s 
Minimum velocity for stable flight reached at: 83.1736 In. 


Max data values:

Maximum acceleration:Vertical (y): 179.316 Ft./s/sHorizontal (x): 0.000 Ft./s/sMagnitude: 179.316 Ft./s/s 
Maximum velocity:Vertical (y): 832.5951 ft/s, Horizontal (x): 5.4725 ft/s, Magnitude: 832.5951 ft/s 
Maximum range from launch site: 634.24869 Ft. 
Maximum altitude: 10395.47246 Ft. 


Recovery system data

P: Parachute Main 1 Deployed at : 26.449 Seconds 
Velocity at deployment: 0.0106 ft/s 
Altitude at deployment: 10395.47246 Ft. 
Range at deployment: 17.72835 Ft. 

Time data

Time to burnout: 7.001 Sec. 
Time to apogee: 26.449 Sec. 
Optimal ejection delay: 19.448 Sec. 
Time to wind shear: 7.409 Sec. 


Landing data

Successful landing 

Time to landing: 242.492 Sec. 
Range at landing: 634.24869 
Velocity at landing: Vertical: -44.9449 ft/s , Horizontal: 0.0000 ft/s , Magnitude: 44.9449 ft/s 


Competition settings

Competition conditions are not in use for this simulation.