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Static Longitudinal Stability and Control Characteristics at a Mach Number of 2.01 of a Hypersonic Missile Configuration Having All-movable Wing and Tail SurfacesStatic longitudinal stability and control characteristics of hypersonic missile configuration with all movable cruciform wing and tail surfaces
Document ID
19650014316
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Foster, G. V. (NASA Langley Research Center Hampton, VA, United States)
Robinson, R. B. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-516
Report Number: NASA-TM-X-516
Accession Number
65N23917
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC VEHICLE
CRUCIFORM WING
MISSILE CONFIGURATION
STATIC STABILITY AND CONTROL
LONGITUDINAL STABILITY AND CONTROL

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