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Flight investigation of the effects of Apollo heat-shield singularities on ablator performanceLaunch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material performance
Document ID
19680025644
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Ohare, B. J. (NASA Langley Research Center Hampton, VA, United States)
Walton, T. E., Jr. (NASA Langley Research Center Hampton, VA, United States)
Witte, W. G. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1968
Subject Category
Thermodynamics And Combustion
Report/Patent Number
NASA-TN-D-4791
Report Number: NASA-TN-D-4791
Accession Number
68N35116
Funding Number(s)
CONTRACT_GRANT: 709-09-00-01-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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