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STATIC LONGTIDUDINAL STABILITY CHARACTERISTICS OF A BLUNTED GLIDER REENTRY CONFIGURATION HAVING 79.5 DEG SWEEPBACK AND 45 DEG DIHEDRAL AT A MACH NUMBER OF 6.2 AND ANGLES OF ATTACK UP TO 20 DEGStatic longitudinal stability characteristics of blunted glider reentry configuration
Document ID
19630002681
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Mayo, E. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-222
Report Number: NASA-TM-X-222
Accession Number
63N12557
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LONGITUDINAL STABILITY
STATIC STABILITY
BLUNT BODY
REENTRY VEHICLE
GLIDER

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