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Engine selection
[Ratt M900H-0]
Launch conditions
Altitude: 2200.000 Ft.
Relative humidity: 70.000 %
Temperature: 70.000 Deg. F
Pressure: 29.921 In. Hg.
Wind speed model: Light (3-7 MPH)
Wind turbulence: Fairly constant speed (0.01)
Wind starts at altitude: 0.000 Ft.
Launch guide angle: -5 Degrees from vertical
Latitude: 48 Degrees north
Launch guide data:
Launch guide length: 72.000 In.
Velocity at launch guide departure: 46.214 ft/s
The launch guide was cleared at : 0.665 Seconds
User specified minimum velocity for stable flight: 43.999 ft/s
Minimum velocity for stable flight reached at: 67.367 In.
Max data values:
Maximum acceleration: Vert: 669.675 Ft./s/s,
Horz: 11.219 Ft./s/s,
Magnitude: 669.676 Ft./s/s
Maximum velocity: Vert: 948.109 ft/s,
Horz: 11.587 ft/s,
Magnitude: 974.648 ft/s
Maximum range from launch site: 3917.487 Ft.
Maximum altitude: 11898.389 Ft.
Engine ejection charge data:
Conditions at engine ejection charge:
Using a delay time of : 0.000 Seconds
Velocity: 656.430 ft/s
Altitude: 7790.843 Ft.
Recovery system data
P: main chute Deployed at : 182.230 Seconds
Velocity at deployment: 66.580 ft/s
Altitude at deployment: 999.978 Ft.
Range at deployment: -457.381 Ft.
P: drogue chute Deployed at : 27.291 Seconds
Velocity at deployment: 125.211 ft/s
Altitude at deployment: 11898.389 Ft.
Range at deployment: -3917.487 Ft.
Time data
Time to burnout: 12.300 Sec.
Time to apogee: 27.291 Sec.
Optimal ejection delay: 14.991 Sec.
Landing data
Successful landing
Time to landing: 244.251 Sec.
Range at landing: 815.626
Velocity at landing: Vert: -19.609 ft/s,
Horz: 9.349 ft/s,
Magnitude: 21.723 ft/s