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
SAE International , 12/05/2016
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$122.00
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.
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 Information
Published:
12/05/2016
File Size:
1 file , 180 KB
Language:
English
Note:
This product is unavailable in Ukraine, Russia, Belarus
