1950•NASA STI Repository (National Aeronautics and Space Administration)Requires access
The longitudinal stability, control effectiveness, and control hinge moment characteristics obtained from a flight investigation of a canard missile configuration at transonic and supersonic speeds
Roy J Niewald, Martin T Moul
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Abstract
A 60 degree delta wing canard missile configuration was flight-tested at the Langley pilotless aircraft research station at Wallops Island, Va. The results include the longitudinal stability derivatives, control effectiveness, drag characteristics, and control-surface hinge-moment characteristics for a Mach number range of 0.7 to 1.45.