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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