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Flight test aerodynamic heating data for the afterbody of the Project Mercury spacecraft with comparisons to available prediction methodsAfterbody heating by Mercury spacecraft during reentry determined from skin temperatures
Document ID
19670020040
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Murphy, J. D.
(Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 3, 2013
Publication Date
June 1, 1967
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-649
Report Number: NASA-CR-649
Accession Number
67N29369
Funding Number(s)
CONTRACT_GRANT: NAS9-3531
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MERCURY CAPSULE
SPACECRAFT REENTRY
AFTERBODY
SKIN TEMPERATURE
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