NASA NTRS · 19900000342
High-Temperature Polyimide Resin
Abstract
Improved polyimide resin used at continuous temperatures up to 700 degrees F (371 degrees C). PMR-II-50, serves as matrix for fiber-reinforced composites. Material combines thermo-oxidative stability with autoclave processability. Used in such turbine engine components as air-bypass ducts, vanes, bearings, and nozzle flaps. Other potential applications include wing and fuselage skins on high-mach-number aircraft and automotive engine blocks and pistons.
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Vanucci, Raymond D., Malarik, Diane C.. 1990-07-01. High-Temperature Polyimide Resin. https://ntrs.nasa.gov/citations/19900000342
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