Full Description

This specification establishes the requirements for a nominal 250 mDF cure epoxy preimpregnated carbon fiber unidirectional tape product.

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.

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.

Product Details:

Published: 09/01/2011