SAE AMS3914

Advanced Composites Prepreg - Nominal 250 Â°F Cure â 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric

SAE International , 09/14/2012

Publisher: SAE

File Format: PDF

$54.00$109.00

Description

Standard By:SAE International , 09/14/2012

Published:09/14/2012

File Size:1 file , 280 KB

Language:English

Note:This product is unavailable in Ukraine, Russia, Belarus

This specification establishes the requirements for a nominal 250 \mDF cure epoxy preimpregnated carbon fiber plain weave fabric product. The prepreg is a plain weave fabric with 12K tows, a nominal fiber areal weight of 193 gsm, and nominal resin content of 42%.

The purpose of this specification is to allow procurement of a defined material corresponding to the statistically derived material properties published in MIL-HDBK-17.

This material is intended for use in laminate applications with a service temperature of -65 to 180 \mDF.

The composite may be used for the manufacture of primary and secondary aircraft structure.