NASA NTRS · 19950022606
Advanced composite structural concepts and materials technologies for primary aircraft structures: Advanced material concepts
Abstract
To achieve acceptable performance and long-term durability at elevated temperatures (350 to 600 F) for high-speed transport systems, further improvements of the high-performance matrix materials will be necessary to achieve very long-term (60,000-120,000 service hours) retention of mechanical properties and damage tolerance. This report emphasizes isoimide modification as a complementary technique to semi-interpenetrating polymer networks (SIPN's) to achieve greater processibility, better curing dynamics, and possibly enhanced thermo-mechanical properties in composites. A key result is the demonstration of enhanced processibility of isoimide-modified linear and thermo-setting polyimide systems.
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Lau, Kreisler S. Y., Landis, Abraham L., Chow, Andrea W., Hamlin, Richard D.. 1993-02-01. Advanced composite structural concepts and materials technologies for primary aircraft structures: Advanced material concepts. https://ntrs.nasa.gov/citations/19950022606
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