ASTM D 792-2008ASTM D 1252-2006ASTM D 2344-1984ASTM D 2734-2009ASTM D 3039-1976ASTM D 3171-2009ASTM D 3171-2011ASTM D 3530-1976ASTM D 3532-1999ASTM D 5379ASTM E 4-2010ASTM E 168-2006DOT/FAA/AR-03-19DOT/FAA/AR-06/10MIL-HDBK-17SACMA SRM 1R-94
适用范围
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. 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.