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

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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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