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An Investigation of Ablation Behavior of Avcoat 5026-39/M over a Wide Range of Thermal EnvironmentsAblation behavior of heat shield of Apollo command module over wide range of thermal environments
Document ID
19690013568
Document Type
Technical Memorandum (TM)
Authors
Crouch, R. K. (NASA Langley Research Center Hampton, VA, United States)
Walberg, G. D. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1969
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TM-X-1778
Accession Number
69N22933
Funding Number(s)
CONTRACT_GRANT: 124-08-03-05-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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