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Wind-tunnel investigation at Mach numbers from 3.0 to 6.8 of the static aerodynamic characteristics of modified Mercury exit and escape capsule configurationsStatic aerodynamic characteristics of modified Mercury exit and escape capsule configurations at Mach numbers 3.0 to 6.8
Document ID
19670022687
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pearson, A. O. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1960
Subject Category
Space Vehicles
Report/Patent Number
NASA-TM-X-324
Report Number: NASA-TM-X-324
Accession Number
67N32016
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STATIC STABILITY
AERODYNAMIC CHARACTERISTICS
ESCAPE CAPSULE
MERCURY PROJECT

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