NASA NTRS · 19860001823
Fabrication process of a high temperature polymer matrix engine duct
Abstract
The process that was used in the molding of an advanced composite outer by-pass duct planned for the F404 engine is discussed. This duct was developed as a potential replacement for the existing titanium duct in order to reduce both the weight and cost of the duct. The composite duct is now going into the manufacturing technology portion of the program. The duct is fabricated using graphite cloth impregnated with the PMR-15 matrix system.
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Pratt, R. D., Wilson, A. J.. 1985-09-01. Fabrication process of a high temperature polymer matrix engine duct. https://ntrs.nasa.gov/citations/19860001823
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