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NASA NTRS · 20020041495

Mechanical Properties and Microstructural Characterization of Particulate Reinforced Diboride Composites for High Temperature Leading Edge Applications

Abstract

Previous 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.

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BibTeXRIS

Ellerby, Donald T., Johnson, Sylvia M., Bull, Jeff, Laub, Bernie, Reuther, James, Kinney, David, Kontinos, Dean, Beckman, Sarah, Stuffle, Kevin, Cull, A. D., Arnold, Jim. 2001-01-01. Mechanical Properties and Microstructural Characterization of Particulate Reinforced Diboride Composites for High Temperature Leading Edge Applications. https://ntrs.nasa.gov/citations/20020041495

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