P1712AD - High Strength Carbon Fiber Reinforced Toughened Epoxy Fabric Prepreg, Atmospheric Pressure Curing

Details Not available for purchase at this time. Document Number: P1712AD Project Initiation: 02-21-2012 Project Number: Revision Number: Sponsor Name: Michael Stuart Title High Strength Carbon Fiber Reinforced Toughened Epoxy Fabric Prepreg, Atmospheric Pressure Curing Scope This specification establishes the requirements for woven continuous high strength modulus carbon fiber fabric impregnated with a modified B-staged toughened epoxy resin intended for cure using atmospheric (vacuum) pressure only Rationale Development of SAE material specification in support of 5320-1 T650 3k 8HS prepreg material qualification, allowable and manufacturing development program generated under DARPA program .

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