Some Effects of Roll Rate on the Longitudinal Stability Characteristics of the Hughes Falcon Missile, ''C'' Configuration, for a Mach Number Range of 1.1 to 1.8 as Determined From Flight Test
Description:
Report discussing testing of a Hughes Falcon missile, C configuration, to determine the stability and control characteristics of the missile while rolling. Information about the time histories, normal force due to angle of attack, pitching moment due to angle of attack, damping, and control effectiveness is provided.
Date:
December 27, 1955
Creator:
Lundstrom, Reginald R. & Baber, Hal T., Jr.
Item Type:
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Partner:
UNT Libraries Government Documents Department