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Performance of five ablation materials as coating for structures in a region of separated flowCommercially available ablation materials for use as thermal protection for sidewalls of advanced air-to-air missiles - protective coatings for structures in separated flow region
Document ID
19660001377
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Clark, L. E. (NASA Langley Research Center Hampton, VA, United States)
Mc Lain, A. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1965
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-TN-D-3093
Report Number: NASA-TN-D-3093
Accession Number
66N10666
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SEPARATED FLOW
PROTECTIVE COATING
THERMAL PROTECTION
AIR TO AIR MISSILE
ABLATING MATERIAL

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