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Evaluation of heat- and blast-protection materialsA program was initiated at the Kennedy Space Center in December 1967 and conducted through December 1969 to evaluate the performance of heat- and blast-protection materials for ground support equipment used during the Apollo/Saturn launches. Materials believed to be generally suitable for heat and blast protection were subjected to launch-exposure tests. Tests were made during the Apollo/Saturn 502, 503, and 505 launches. Tests were also made in a local laboratory, as an alternative to the restrictive requirements of launch-exposure tests, to determine the effects of torch-flame exposure on ablative materials. Five materials were found to be satisfactory in all major test categories. It was determined that torch-flame tests can probably be utilized as an acceptable substitute for the booster-engine-exhaust exposure tests for basic screening of candidate materials.
Document ID
19720005290
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Morrison, J. D.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Lockhart, B. J.
(NASA John F. Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1971
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-6484
Report Number: NASA-TN-D-6484
Accession Number
72N12939
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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