AMS3970/2: Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive - Material Specification

Features

Issuing Committee: AMS CACRC Commercial Aircraft Composite Repair Committee

Scope

Content: AMS 3970/2 gives specific information about the qualification program for carbon fiber reinforced epoxy structural repair prepreg systems, applicable for 125 °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.

Meta Tags

Topics: Materials properties
Fibers
Fabrics and textiles
Adhesives and sealants
Composite materials
Resins
Thermoplastics
Drying
Vacuum

Details

DOI: https://doi.org/10.4271/AMS3970/2

Pages: 17

Citation: SAE International Material Specification, Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 2 - Qualification Program for Fiber, Fabric, Resin and Film Adhesive, SAE Standard AMS3970/2, Issued December 1999, https://doi.org/10.4271/AMS3970/2.

Additional Details

Publisher: SAE International

Published: Dec 1, 1999

Product Code: AMS3970/2

Content Type: Material Specification

Status: Issued

Language: English

Historical