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. The properties of 8 different graphite composite panels fabricated using four different resin matrices and two types of graphite reinforcement are described. The resin matrices included: XU71775/H795, a blend of vinyl polystyryl pyridine and bismaleimide; H795, a bismaleimide; Cycom 6162, a phenolic; and PSP 6022M, a polystyryl pyridine....
Results are presented from an experimental evaluation of IM7/8551-7 and IM6/18081, two new toughened...
This work and a predecessor investigation form a two-part experimental research program on the effec...
High temperature resin matrices suitable for use in advanced graphite fiber composites for jet engin...
The properties of eight different graphite composite panels fabricated using four different resin ma...
This article looks at the effect of different resin matrices on thermal and mechanical properties of...
Eight different graphite composite panels were fabricated using four different resin matrices. The r...
Eight different graphite composite panels were fabricated using four different resin matrices. The r...
The successful fabrication of high temperature resistant composites depends mainly on the processabi...
Graphite fiber reinforced resin matrix composites were subjected to controlled burning conditions to...
The thermochemical and flammability characteristics of two polymeric composites currently in use and...
Survey visits to companies involved in the manufacture and use of graphite-epoxy prepregs were condu...
A broad group of fibers and matrices were combined to create a wide range of composite properties. P...
Vinystilbazole (vinylstryrylpyridine) and vinylpolystyrulpyridine were prepared for the purpose of m...
This first part of a series of papers on the thermo-mechanical responses of fiber-reinforced composi...
A commercial two-components epoxy resin formulation was successfully modified by adding graphene and...
Results are presented from an experimental evaluation of IM7/8551-7 and IM6/18081, two new toughened...
This work and a predecessor investigation form a two-part experimental research program on the effec...
High temperature resin matrices suitable for use in advanced graphite fiber composites for jet engin...
The properties of eight different graphite composite panels fabricated using four different resin ma...
This article looks at the effect of different resin matrices on thermal and mechanical properties of...
Eight different graphite composite panels were fabricated using four different resin matrices. The r...
Eight different graphite composite panels were fabricated using four different resin matrices. The r...
The successful fabrication of high temperature resistant composites depends mainly on the processabi...
Graphite fiber reinforced resin matrix composites were subjected to controlled burning conditions to...
The thermochemical and flammability characteristics of two polymeric composites currently in use and...
Survey visits to companies involved in the manufacture and use of graphite-epoxy prepregs were condu...
A broad group of fibers and matrices were combined to create a wide range of composite properties. P...
Vinystilbazole (vinylstryrylpyridine) and vinylpolystyrulpyridine were prepared for the purpose of m...
This first part of a series of papers on the thermo-mechanical responses of fiber-reinforced composi...
A commercial two-components epoxy resin formulation was successfully modified by adding graphene and...
Results are presented from an experimental evaluation of IM7/8551-7 and IM6/18081, two new toughened...
This work and a predecessor investigation form a two-part experimental research program on the effec...
High temperature resin matrices suitable for use in advanced graphite fiber composites for jet engin...