SAE AMS3960

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

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Standard:
  • AMS3960
Issued:
  • 2011-09-01
Issuing:
  • Ams P17 Composite Materials Committee
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.

History:
StandardPublishedRevisionStatus
AMS39602011-09-01LatestIssued
AKA:
  • SAE AMS 3960
Sector:
  • Aerospace
Topic:
  • Materials
  • Composite materials
  • Fabrics
  • Fibers
  • Glass
  • Lightweight materials
  • Resins
  • Materials properties

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