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About This Item

 

Full Description

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.
 

Document History

  1. SAE AMS3914A


    Advanced Composites Prepreg ¿¿¿ Nominal 250 ¿¿F Cure ¿¿¿ 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric

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  2. SAE AMS3914

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

    • Historical Version