Property data reported is normalized to 60% fiber volume. Cured with #2592 epoxy at 130 °C. Intermediate modulus, high tensile strength fiber, with excellent balanced composite properties. Designed and developed to meet the weight saving demand of aircraft. Excellent processability in traditional manufacturing methods (weaving, braiding, filament winding, prepreg, etc.) Information provided by Toray Composite Materials America, Inc. |