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NASA NTRS · 19960052323

Graphite Fiber Textile Preform/Copper Matrix Composites

Abstract

Graphite fiber reinforced/copper matrix composites are candidate materials for critical heat transmitting and rejection components because of their high thermal conduction. The use of textile (braid) preforms allows near-net shapes which confers additional advantages, both for enhanced thermal conduction and increased robustness of the preform against infiltration and handling damage. Issues addressed in the past year center on the determination of the braid structure following infiltration, and the braidability vs. the conductivity of the fibers. Highly conductive fibers eventuate from increased graphitization, which increases the elastic modulus, but lowers the braidability; a balance between these factors must be achieved. Good quality braided preform bars have been fabricated and infiltrated, and their thermal expansion characterized; their analytic modeling is underway. The braided preform of an integral finned tube has been fabricated and is being prepared for infiltration.

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BibTeXRIS

Filatovs, G. J., Lee, Bruce, Bass, Lowell. 1996-07-01. Graphite Fiber Textile Preform/Copper Matrix Composites. https://ntrs.nasa.gov/citations/19960052323

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