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Analytical Micromechanics Modeling Technique Developed for Ceramic Matrix Composites Analysis (2005)

Min, James B.

In: CASI

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Publication Date: 2018-06-05

Description: Ceramic matrix composites (CMCs) promise many advantages for next-generation aerospace propulsion systems. Specifically, carbon-reinforced silicon carbide (C/SiC) CMCs enable higher operational temperatures and provide potential component weight savings by virtue of their high specific strength. These attributes may provide systemwide benefits. Higher operating temperatures lessen or eliminate the need for cooling, thereby reducing both fuel consumption and the complex hardware and plumbing required for heat management. This, in turn, lowers system weight, size, and complexity, while improving efficiency, reliability, and service life, resulting in overall lower operating costs.

Keywords: Composite Materials

Type: Research and Technology 2004; NASA/TM-2005-213419

Format: application/pdf

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