Big Daddy - Simulation results

Engine selection

[E9-6]

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: 0.00000 Ft.
• Relative humidity: 50.000 %
• Temperature: 59.000 Deg. F
• Pressure: 29.9139 In.

Wind speed model: Calm (0-2 MPH)

• Low wind speed: 0.0000 MPH
• High wind speed: 2.0000 MPH

Wind turbulence: Fairly constant speed (0.01)

• Frequency: 0.010000 rad/second
• Wind starts at altitude: 0.00000 Ft.
• Launch guide angle: 0.000 Deg.
• Latitude: 0.000 Degrees

Launch guide data:

• Launch guide length: 36.0000 In.
• Velocity at launch guide departure: 31.7323 ft/s
• The launch guide was cleared at : 0.316 Seconds
• User specified minimum velocity for stable flight: 43.9993 ft/s
• Minimum velocity for stable flight reached at: 85.4664 In.

Max data values:

• Maximum acceleration:Vertical (y): 198.928 Ft./s/sHorizontal (x): 4.339 Ft./s/sMagnitude: 198.928 Ft./s/s
• Maximum velocity:Vertical (y): 203.6454 ft/s, Horizontal (x): 2.7982 ft/s, Magnitude: 204.8588 ft/s
• Maximum range from launch site: 121.86727 Ft.
• Maximum altitude: 768.95422 Ft.

Engine ejection charge data:

• Using a delay time of : 6.000 Seconds
• Velocity: 43.0319 ft/s
• Altitude: 741.93179 Ft.

Recovery system data

• P: Parachute Deployed at : 9.090 Seconds
• Velocity at deployment: 43.0319 ft/s
• Altitude at deployment: 741.93179 Ft.
• Range at deployment: -121.86727 Ft.

Time data

• Time to burnout: 3.090 Sec.
• Time to apogee: 7.782 Sec.
• Optimal ejection delay: 4.692 Sec.

Landing data

• Successful landing
• Time to landing: 44.149 Sec.
• Range at landing: -28.45817
• Velocity at landing: Vertical: -20.5532 ft/s , Horizontal: 2.7982 ft/s , Magnitude: 20.7428 ft/s

Competition settings

Competition conditions are not in use for this simulation.