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AMS3960A - Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape

Details
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Document Number: AMS3960A
Project Initiation: 04-15-2013
Project Number:
Revision Number: A
Sponsor Name: Damon Call
Title
Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape
Scope
<p>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. </p>
Rationale
<p>Widely distributed and available industry material specifications are required for procurement of composite materials whose allowables data is published in CMH-17.</p>
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