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Development of techniques and associated instrumentation for high temperature emissivity measurementsStudies were made to develop a test apparatus for the measurement of total emittance of materials under repeated exposure to simulated earth entry conditions. As no existing test facility met the emittance measurement and entry simulation goals, a new apparatus was designed, fabricated and checked out. This apparatus has the capability of performing total and spectral emittance measurements during cyclic temperature and pressure exposure under sonic and supersonic flow conditions. Emittance measurements were performed on a series of oxidized superalloys, silicide coated columbium alloys and ceramic coatings.
Document ID
19730023607
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Cunnington, G. R.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Funaa, A. I.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Cassady, P. E.
(Lockheed Missiles and Space Co. Palo Alto, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1973
Subject Category
Instrumentation And Photography
Report/Patent Number
NASA-CR-124423
LMSC-D352380
Report Number: NASA-CR-124423
Report Number: LMSC-D352380
Accession Number
73N32339
Funding Number(s)
CONTRACT_GRANT: NAS8-26304
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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