Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape

Standard:
Issued:
  • 2011-09-01
 
  • HISTORICAL Access the latest revision: AMS3960A
Publisher:
  • SAE International
Pages:
25
Scope:

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.

Rationale:

Widely distributed and available industry material specifications are required for procurement of composite materials whose allowables data is published in MIL-HDBK-17.

History:
Standard Published Revision Status
AMS3960A 2015-08-11 Latest Revised
2011-09-01 Historical Issued
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