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An Experimental Investigation of the Static Longitudinal Stability and Control Characteristics of a Wingless Missile Configuration at Mach Numbers from 3.0 to 6.3Static longitudinal stability and control characteristics of wingless missile configuration at supersonic and hypersonic speeds
Document ID
19650003101
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Gloria, H. R. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 24, 1958
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A58C20
Report Number: NACA-RM-A58C20
Accession Number
65N12702
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
WINGLESS VEHICLE
STATIC STABILITY
LONGITUDINAL STABILITY AND CONTROL
MISSILE CONFIGURATION

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