SAE AMS3960-2011 PDF

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. 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.

SAE AMS3960-2011 Referenced Document

ASTM D1252-06 Standard Test Methods for Chemical Oxygen Demand (Dichromate Oxygen Demand) of Water*， 2024-04-19 Update
ASTM D2734-09 Standard Test Methods for Void Content of Reinforced Plastics*， 2024-04-19 Update
ASTM D3171-09 Standard Test Methods for Constituent Content of Composite Materials*， 2024-04-19 Update
ASTM D3171-11 Standard Test Methods for Constituent Content of Composite Materials*， 2024-04-19 Update
ASTM D3532-99 Standard Test Method for Gel Time of Carbon Fiber-Epoxy Prepreg
ASTM D5379
ASTM D792-08 Standard Test Methods for Density and Specific Gravity (Relative Density) of Plastics by Displacement*， 2024-04-19 Update
ASTM E168-06 Standard Practices for General Techniques of Infrared Quantitative Analysis *， 2024-04-19 Update
ASTM E4-10 Standard Practices for Force Verification of Testing Machines*， 2024-04-19 Update

2015 SAE AMS3960A-2015 Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape
2011 SAE AMS3960-2011 Advanced Composites Prepreg - Nominal 250 °F Cure - Carbon Fiber and Epoxy Resin, Unidirectional Tape