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
