NASA NTRS · 19810019624
Advanced resin systems for graphite epoxy composites
Abstract
The value of resin/carbon fiber composites as lightweight structures for aircraft and other vehicle applications is dependent on many properties: environmental stability, strength, toughness, resistance to burning, smoke produced when burning, raw material costs, and complexity of processing. A number of woven carbon fiber and epoxy resin composites were made. The epoxy resin was commercially available tetraglycidylmethylene dianiline. In addition, composites were made using epoxy resin modified with amine and carboxyl terminated butadiene acrylonitrile copolymer. Strength and toughness in flexure as well as oxygen index flammability and NBS smoke chamber tests of the composites are reported.
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Gilwee, W. J., Jayarajan, A.. 1980-01-01. Advanced resin systems for graphite epoxy composites. https://ntrs.nasa.gov/citations/19810019624
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