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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
