NASA NTRS · 19900000463
Process For Autoclaving HMW PMR-II Composites
Abstract
Parts made of graphite-reinforced, high-molecular-weight (HMW) PMR-II polyimide easy to fabricate by autoclaving. Study showed autoclaved HMW PMR-II parts equal in quality to those made by compression molding. Well suited to use at temperatures up to 700 degrees F (371 degrees C). In aircraft engines, they offer advantages of strength and light weight.
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Vannucci, Raymond D., Cifani, Diane. 1990-09-01. Process For Autoclaving HMW PMR-II Composites. https://ntrs.nasa.gov/citations/19900000463
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