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Emissivity Results on High Temperature Coatings for Refractory Composite MaterialsThe directional emissivity of various refractory composite materials considered for application for reentry and hypersonic vehicles was investigated. The directional emissivity was measured at elevated temperatures of up to 3400 F using a directional spectral radiometric technique during arc-jet test runs. A laboratory-based relative total radiance method was also used to measure total normal emissivity of some of the refractory composite materials. The data from the two techniques are compared. The paper will also compare the historical database of Reinforced Carbon-Carbon emissivity measurements with emissivity values generated recently on the material using the two techniques described in the paper.
Document ID
20070031768
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Ohlhorst, Craig W.
(NASA Langley Research Center Hampton, VA, United States)
Vaughn, Wallace L.
(NASA Langley Research Center Hampton, VA, United States)
Daryabeigi, Kamran
(NASA Langley Research Center Hampton, VA, United States)
Lewis, Ronald K.
(NASA Johnson Space Center Houston, TX, United States)
Rodriguez, Alvaro C.
(NASA Johnson Space Center Houston, TX, United States)
Milhoan, James D.
(Mei Technology Corp. United States)
Koenig, John R.
(Southern Research Inst. Birmingham, AL, United States)
Date Acquired
August 23, 2013
Publication Date
June 24, 2007
Subject Category
Composite Materials
Meeting Information
Meeting: 29th International Thermal Conductivity Conference (ITCC) and 17th International Expansion Symposium
Location: Birmingham, AL
Country: United States
Start Date: June 24, 2007
End Date: June 27, 2007
Funding Number(s)
WBS: WBS 599489.02.07.07.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
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