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Entry Performance of the Mercury Spacecraft Heat ShieldFlight performance characteristics of Mercury capsule ablative heat shield
Document ID
19660006061
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Erb, R. B.
Jacobs, S.
Date Acquired
September 2, 2013
Publication Date
January 1, 1964
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-57097
Accession Number
66N15350
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HEAT SHIELD
AIRCRAFT PERFORMANCE
MERCURY CAPSULE
PERFORMANCE CHARACTERISTICS
ABLATING MATERIAL

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