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

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.

Product Details

Published:

12/05/2016

File Size:

1 file 180 KB

Note:

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