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Static longitudinal, directional, and lateral stability and control data at a Mach number of 6.83 of the final configuration of the X- 15 research airplaneX-15 aircraft static longitudinal, directional, and lateral stability and control at hypersonic speeds
Document ID
19660024030
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Fetterman, D. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Penland, J. A. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1960
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-236
Report Number: NASA-TM-X-236
Accession Number
66N33320
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC SPEED
LATERAL STABILITY AND CONTROL
STATIC STABILITY AND CONTROL
DIRECTIONAL STABILITY
LONGITUDINAL STABILITY AND CONTROL
X-15 AIRCRAFT

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