SAE AMS3970/1A

Anotace textu normy SAE AMS3970/1A :

AMS3970/1 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.

SUBJECT TAXONOMY: Maintenance and Aftermarket, Maintenance, repair, and service operations, Materials, Composite materials
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Material Specification