SAE AMS3970/6

Detailinformationen

Bezeichnung: SAE AMS3970/6

Ausgabedatum: 01.12.2016

Seiten: 0

Land: Amerikanische technische Norm

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Annotation

This Material Specification defines the requirements of carbon fiber reinforced epoxy prepreg for repair, 120 °C (250 °F) Vacuum curing, Plain Weave Fabric, 193 g/m2 and a companion non-structural glass fiber fabric reinforced epoxy prepreg, 105 g/m2, qualified according to AMS3970/1 and AMS3970/2 for aerospace application.

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. If included, the requirements to be met by the adhesive are also defined in this document.

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