- Simulation results

Engine selection

[H400-Vmax-7]

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: 1000.00000 Ft.
  • Relative humidity: 50.000 %
  • Temperature: 50.000 Deg. F
  • Pressure: 29.9139 In.
  • Wind speed model: Slightly breezy (8-14 MPH)

    • Low wind speed: 8.0000 MPH
    • High wind speed: 14.9000 MPH

    Wind turbulence: Fairly constant speed (0.01)

    • Frequency: 0.010000 rad/second
  • Wind starts at altitude: 0.00000 Ft.
  • Launch guide angle: 0.001 Deg.
  • Latitude: 40.000 Degrees

Launch guide data:

  • Launch guide length: 96.0000 In.
  • Velocity at launch guide departure: 78.2044 ft/s
  • The launch guide was cleared at : 0.225 Seconds
  • User specified minimum velocity for stable flight: 43.9993 ft/s
  • Minimum velocity for stable flight reached at: 33.5579 In.

Max data values:

  • Maximum acceleration:Vertical (y): 423.612 Ft./s/sHorizontal (x): 0.755 Ft./s/sMagnitude: 423.649 Ft./s/s
  • Maximum velocity:Vertical (y): 242.6027 ft/s, Horizontal (x): 19.7616 ft/s, Magnitude: 243.2171 ft/s
  • Maximum range from launch site: 430.57588 Ft.
  • Maximum altitude: 867.77559 Ft.

Engine ejection charge data:

  • Using a delay time of : 7.000 Seconds
  • Velocity: 15.7053 ft/s
  • Altitude: 867.40639 Ft.

Recovery system data

  • P: Parachute Deployed at : 7.641 Seconds
  • Velocity at deployment: 15.7053 ft/s
  • Altitude at deployment: 867.40639 Ft.
  • Range at deployment: -80.71985 Ft.

Time data

  • Time to burnout: 0.641 Sec.
  • Time to apogee: 7.491 Sec.
  • Optimal ejection delay: 6.850 Sec.

Landing data

  • Successful landing
  • Time to landing: 34.294 Sec.
  • Range at landing: 430.57588
  • Velocity at landing: Vertical: -33.0559 ft/s , Horizontal: 19.7616 ft/s , Magnitude: 38.5125 ft/s
.