AMS3960B: Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape - Material Specification

Features

Issuing Committee: AMS P17 Polymer Matrix Composites Committee

Scope

Content: The intent of this specification is for the procurement of carbon fiber epoxy prepreg product with 250 °F (121 °C) cure for aerospace applications; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the production quality assurance section (see 4.3).

Meta Tags

Topics: Carbon fibers
Materials properties
Composite materials

Details

DOI: https://doi.org/10.4271/AMS3960B

Citation: SAE International Material Specification, Advanced Composites Prepreg - Nominal 250 °F (121 °C) Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape, SAE Standard AMS3960B, Revised May 2026, Issued September 2011, https://doi.org/10.4271/AMS3960B.

Additional Details

Publisher: SAE International

Published: May 15

Product Code: AMS3960B

Content Type: Material Specification

Status: Revised

Language: English

Historical