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Development of Ablation Sensors for Advanced Reentry VehiclesDesign and operation of make wire, light pipe, and spring wire sensors to measure in-flight thermal parameters of ablative reentry vehicle heat shield
Document ID
19660020065
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Le Bel, P. J. (NASA Langley Research Center Hampton, VA, United States)
Russell, J. A., III (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1965
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-TM-X-56771
Report Number: NASA-TM-X-56771
Accession Number
66N29355
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ABLATING MATERIAL
REENTRY VEHICLE
HEAT SHIELD
SENSOR

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