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Development of sensors to obtain in-flight ablation measurements of thermal-protection materialsDesign and development of sensors for measuring ablative changes in space vehicle heat shield during reentry phase
Document ID
19660030245
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Le Bel, P. J. (NASA Langley Research Center Hampton, VA, United States)
Russell, J. M., III (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1966
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TN-D-3686
Report Number: NASA-TN-D-3686
Accession Number
66N39535
Funding Number(s)
CONTRACT_GRANT: 125-24-03-08-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ABLATION
SPACECRAFT REENTRY
SENSOR
HEAT SHIELD

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