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Wind-tunnel Investigation at a Mach Number of 2.91 of Stability and Control Characteristics of Three Lifting Reentry Configurations at Angles of Attack up to 90 DegreesStability and control characteristics of reentry vehicle configurations at angles of attack up to 90 deg, in wind tunnel at Mach number 2.91
Document ID
19660024016
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Grimaud, J. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-455
Report Number: NASA-TM-X-455
Accession Number
66N33306
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
WIND TUNNEL
REENTRY VEHICLE
ANGLE OF ATTACK

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