SAE AMS3970/6
- Carbon Fiber Fabric Repair Prepreg, 120 ¿¿C (250 ¿¿F) Vacuum Curing Part 6 - Material Specification: Carbon Fiber Fabric Reinfor
- standard by SAE International, 12/05/2016
- Category: SAE
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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/m\u2 and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m\u2, 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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