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WIND-TUNNEL INVESTIGATION AT MACH NUMBERS FROM 0.30 TO 1.14 OF THE STATIC AERODYNAMIC CHARACTERISTICS OF MODIFIED MERCURY ESCAPE AND EXIT CAPSULE CONFIGURATIONSStatic aerodynamic characteristics of modified mercury escape and exit capsule configurations at mach numbers 0.30 to 1.4
Document ID
19630010659
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pearson, A. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1961
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-547
Report Number: NASA-TM-X-547
Accession Number
63N20539
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MERCURY CAPSULE
ESCAPE CAPSULE
STATIC AERODYNAMIC CHARACTERISTICS

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