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THE LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A RE-ENTRY CONFIGURATION BASED ON A BLUNT 13 DEG HALF-CONE AT MACH NUMBERS TO 0.92Longitudinal aerodynamic characteristics of blunt, lifting reentry vehicle at mach 0.92
Document ID
19630010661
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kenyon, G. C. (NASA Ames Research Center Moffett Field, CA, United States)
Sutton, F. B. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1961
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-571
Report Number: NASA-TM-X-571
Accession Number
63N20541
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
BLUNT BODY
LONGITUDINAL STABILITY AND CONTROL
REENTRY VEHICLE
LIFTING REENTRY
AERODYNAMIC CHARACTERISTICS

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