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Mechanical Properties and Microstructural Characterization of Particulate Reinforced Diboride Composites for High Temperature Leading Edge ApplicationsPrevious work on refractory diboride composites has shown that these systems have the potential for use in high temperature leading edge applications for reusable reentry vehicles. Experiments in reentry environments have shown that these materials have multiple use temperatures greater than 1900 C. The work to be discussed focuses on three compositions: HfB2/SiC, ZrB2/SiC, and ZrB2/C/SiC. These composites have been hot pressed and their mechanical properties measured at room and elevated temperatures. Extensive microstructural characterization has been conducted on polished cross sections and the fracture surfaces have been examined to determine their failure origins.
Document ID
20010097944
Acquisition Source
Ames Research Center
Document Type
Abstract
Authors
Ellerby, Donald T.
(NASA Ames Research Center Moffett Field, CA United States)
Bull, J. D.
(NASA Ames Research Center Moffett Field, CA United States)
Johnson, S. M.
(NASA Ames Research Center Moffett Field, CA United States)
Stackpoole, M. M.
(Eloret Corp. Sunnyvale, CA United States)
Gusman, M.
(Eloret Corp. Sunnyvale, CA United States)
Stuffle, K.
(Materials and Machines Co. Tucson, AZ United States)
Cull, A. D.
(Southern Research Inst. Birmingham, AL United States)
Causey, S. J.
(Southern Research Inst. Birmingham, AL United States)
Arnold, Jim
Date Acquired
August 20, 2013
Publication Date
January 21, 2001
Subject Category
Composite Materials
Meeting Information
Meeting: Pacific Rim IV International Conference
Location: Wailea, HI
Country: United States
Start Date: November 4, 2001
End Date: November 8, 2001
Sponsors: American Ceramic Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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