AMS3970/1: Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 1 - General Requirements - Material Specification

Features

Issuing Committee: AMS CACRC Commercial Aircraft Composite Repair Committee

Scope

Content: AMS 3970/1 gives information about the technical requirements and qualification procedure for carbon fiber fabric epoxy 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.

Meta Tags

Topics: Materials properties
Composite materials
Heat resistant materials
Coatings, colorants, and finishes
Fabrics and textiles
Production
Adhesives and sealants
Fibers
Manufacturing processes

Details

DOI: https://doi.org/10.4271/AMS3970/1

Pages: 40

Citation: SAE International Material Specification, Carbon Fiber Fabric Repair Prepreg, 125 °C (250 °F) Vacuum Curing Part 1 - General Requirements, SAE Standard AMS3970/1, Issued December 1999, https://doi.org/10.4271/AMS3970/1.

Additional Details

Publisher: SAE International

Published: Dec 1, 1999

Product Code: AMS3970/1

Content Type: Material Specification

Status: Issued

Language: English

Historical