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A study for development of aerothermodynamic test model materials and fabrication techniqueA literature survey, materials reformulation and tailoring, fabrication problems, and materials selection and evaluation for fabricating models to be used with the phase-change technique for obtaining quantitative aerodynamic heat transfer data are presented. The study resulted in the selection of two best materials, stycast 2762 FT, and an alumina ceramic. Characteristics of these materials and detailed fabrication methods are presented.
Document ID
19720023302
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Dean, W. G.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Connor, L. E.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Publication Information
Publisher: NASA
Subject Category
Thermodynamics And Combustion
Report/Patent Number
HREC-9983-1
NASA-CR-2065
Report Number: HREC-9983-1
Report Number: NASA-CR-2065
Accession Number
72N30952
Funding Number(s)
CONTRACT_GRANT: NAS1-9983
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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