Description

This specification establishes the requirements for a nominal 250 °F 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 °F. The composite may be used for the manufacture of primary and secondary aircraft structure.

Product Details

Published:

08/11/2015

File Size:

1 file , 370 KB

Redline File Size:

2 files , 3.2 MB