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NASA NTRS · 19960018788

Computer-Aided Process Model For Carbon/Phenolic Materials

Abstract

Computer program implements thermochemical model of processing of carbon-fiber/phenolic-matrix composite materials into molded parts of various sizes and shapes. Directed toward improving fabrication of rocket-engine-nozzle parts, also used to optimize fabrication of other structural components, and material-property parameters changed to apply to other materials. Reduces costs by reducing amount of laboratory trial and error needed to optimize curing processes and to predict properties of cured parts.

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BibTeXRIS

Letson, Mischell A., Bunker, Robert C.. 1996-03-01. Computer-Aided Process Model For Carbon/Phenolic Materials. https://ntrs.nasa.gov/citations/19960018788

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