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A study of the effects of environmental and ablator performance uncertainties on heat shielding requirements for hyperbolic entry vehicles. Volume 2 - Summary of calculationsCalculated ablative quantities for nylon phenolic heat shielding materials of hyperbolic reentry vehicles
Document ID
19680015517
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chin, J. H. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Coleman, W. D. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Gallagher, L. W. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Hearne, L. F. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Lefferdo, J. M. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 4, 2013
Publication Date
January 1, 1968
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-CR-73225
Accession Number
68N24989
Funding Number(s)
CONTRACT_GRANT: NAS2-4219
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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