(R) Advanced Composites Prepreg - Nominal 250 °F Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric
|Publication Date:||1 September 2015|
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%.
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.