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SAE AMS3914

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

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Organization: SAE
Publication Date: 1 September 2015
Status: active
Page Count: 29
scope:

Form

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%.

Purpose

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

b. This material is intended for use in laminate applications with a service temperature of -65 °F to 180 °F.

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

Document History

SAE AMS3914
September 1, 2015
(R) Advanced Composites Prepreg - Nominal 250 °F Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric
Form 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...
September 1, 2012
Advanced Composites Prepreg – Nominal 250 °F Cure – 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric
Form 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...

References

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