Carbon Fiber Fabric Repair Prepreg, 120 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Carbon Prepreg, Film Adhesive and Non-Structural Glass Prepreg
STANDARD published on 1.12.2016
Designation standards: SAE AMS3970/2A
Publication date standards: 1.12.2016
Country: American technical standard
Category: Technical standards SAE
AMS3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 120 °C (250 °F) vacuum curing. 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.
SUBJECT TAXONOMY: Maintenance and Aftermarket, Maintenance, repair, and service operations, Materials, Composite materials
SUBFILE: Aerospace
TYPE OF DOCUMENT: Aerospace Material Specification