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Carbon Fiber Fabric Repair Prepreg, 120 ¿¿C (250 ¿¿F) Vacuum Curing Part 1 – General Requirements
standard by SAE International, 12/06/2016
Description
AMS 3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy prepreg and a companion non-structural glass prepreg used for repair of carbon fiber reinforced epoxy structures. The prepreg system may include a 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.
Product Details
- Published:
- 12/06/2016
- File Size:
- 1 file , 230 KB