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Flight-determined stability and control characteristics of the M2-F3 lifting body vehicle

Alex G. Sim

Abstract

Flight data were obtained over a Mach number range from 0.4 to 1.55 and an angle-of-attack range from -2 deg to 16 deg. Lateral-directional and longitudinal derivatives, reaction control rocket effectiveness, and longitudinal trim information obtained from flight data and wind-tunnel predictions are compared. The effects of power, configuration change, and speed brake are discussed.

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Available abstract

Key concepts: Trim, Longitudinal static stability, Mach number, Angle of attack, Range (aeronautics), Aerospace engineering, Rocket (weapon), Brake