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INVESTIGATION OF THE LOW-SUBSONIC STABILITY AND CONTROL CHARACTERISTICS OF A 1 3-SCALE FREE-FLYING MODEL OF A LIFTING-BODY REENTRY CONFIGURATIONFree flying 1/3-scale model of a lifting reentry configuration and low subsonic stability and control characteristics
Document ID
19630004024
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hassell, J. L., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1960
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-X-297
Report Number: NASA-TM-X-297
Accession Number
63N13900
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIFTING REENTRY
REENTRY VEHICLE
STABILITY AND CONTROL

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