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Surface emissivity of a reinforced carbon composite material with an oxidation-inhibiting coatingTotal effective emissivity and spectral emissivity over the wavelength range of 0.65 to 6.3 microns were determined for temperatures from 1300 t0 2250 deg K. A multi channel radiometer was used in the arcjet and laboratory tests. The black-body-hole method was used to independently check radiometer results. The results show the silicon-carbide coated reinforced carbon composite material is a nongray radiator. The total effective emissivity and the spectral emissivity at 0.65 micron both decreased with increasing temperature, respectively, from approximately 0.8 to 0.6, and from 0.4 to 0.25, over the temperature range. The emissivity values were the same when the sample was viewed normal to the surface or at a 45 deg angle. Recommended emissivity values are presented.
Document ID
19740004171
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Wakefield, R. M.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1973
Subject Category
Materials, Nonmetallic
Report/Patent Number
NASA-TM-X-62315
Report Number: NASA-TM-X-62315
Accession Number
74N12284
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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