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

Standard:
Issued:
  • 2012-09-14
 
  • HISTORICAL Access the latest revision: AMS3914A
Publisher:
  • SAE International
Pages:
24
Scope:

This specification establishes the requirements for a nominal 250 °F 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 °F.

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

Rationale:

Widely distributed and available industry material specifications are required for procurement of composite materials whose allowables data is published in MIL-HDBK-17.

History:
Standard Published Revision Status
AMS3914A 2015-09-03 Latest Revised
2012-09-14 Historical Issued
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