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Preliminary evaluation of adhesion strength measurement devices for ceramic/titanium matrix composite bondsThe adhesive bond between ceramic cement and a titanium matrix composite substrate to be used in the National Aerospace Plane program is evaluated. Two commercially available adhesion testers, the Sebastian Adherence Tester and the CSEM REVETEST Scratch Tester, are evaluated to determine their suitability for quantitatively measuring adhesion strength. Various thicknesses of cements are applied to several substrates, and bond strengths are determined with both testers. The Sabastian Adherence Tester has provided limited data due to an interference from the sample mounting procedure, and has been shown to be incapable of distinguishing adhesion strength from tensile and shear properties of the cement itself. The data from the scratch tester has been found to be difficult to interpret due to the porosity and hardness of the cement. Recommendations are proposed for a more reliable adhesion test method.
Document ID
19920022023
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pohlchuck, Bobby
(Kent State Univ. OH., United States)
Zeller, Mary V.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1992
Subject Category
Aeronautics (General)
Report/Patent Number
NAS 1.15:105803
E-7233
NASA-TM-105803
Report Number: NAS 1.15:105803
Report Number: E-7233
Report Number: NASA-TM-105803
Accession Number
92N31267
Funding Number(s)
CONTRACT_GRANT: NCC3-189
PROJECT: RTOP 763-22-51
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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