NASA NTRS ยท 19880049142
Bismaleimide-vinylpolystyrylpyridine graphite composites
Abstract
Flammability, thermal, and selected mechanical properties of composites fabricated with epoxy and other thermally stable resin matrices are described. Properties which were measured included limiting-oxygen index, smoke evolution, thermal degradation products, total-heat release, heat-release rates, mass loss, flame spread, ignition resistance, thermogravimetric analysis and selected mechanical properties. This paper describes the properties of eight different graphite composite panels fabricated using four different resin matrices and two types of graphite reinforcement. The resin matrices included: XU71775/H795, a blend of vinylpolystyrylpyridine and bismaleimide; H795, a bismaleimide; Cycom 6162, a phenolic; and PSP 6022M, a polystyrylpyridine. The graphite fiber used was AS-4 in the form of either tape or fabric. The properties of these composites were compared with epoxy composites. It was determined that the blend of vinylpolystyrylpyridine and bismaleimide (XU71775/H795) with the graphite tape was the optimum design giving the lowest heat release rate.
Keep this discovery
Explore connections, maps & timelines
Kourtides, D. A.. 1988-01-01. Bismaleimide-vinylpolystyrylpyridine graphite composites. https://ntrs.nasa.gov/citations/19880049142
Cite the original work for its findings. Save a collection to share your selection of sources.