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SAE AMS3970/6

SAE AMS3970/6 Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 6 - Material Specification: Carbon Fiber Fabric Reinforced Epoxy Prepreg for Repair, Plain Weave Fabric, 193 g/m2, Adhesive Film for Repair and Non-Structural Glass Fiber Fabric Reinforced Epoxy Prepreg, 105 g/m2

standard by SAE International, 12/05/2016

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This Material Specification defines the requirements of carbon fiber reinforced epoxy prepreg for repair, 120 mDC (250 mDF) Vacuum curing, Plain Weave Fabric, 193 g/mu2 and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/mu2, qualified according to AMS3970/1 and AMS3970/2 for aerospace application.

The prepreg system may include an epoxy film adhesive to be applied in a co-curing process with the prepreg for joint and sandwich bonding. The need for a film adhesive shall be established during screening tests. If included, the requirements to be met by the adhesive are also defined in this document.

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Published: 12/05/2016File Size: 1 file , 180 KB