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

File Size:

1 file , 700 KB