SAE AMS3914
Advanced Composites Prepreg - Nominal 250 °F Cure – 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric.
Standard:
AKA:
- AMS3914
- 2012-09-14
- Ams P17 Composite Materials Committee
This specification establishes the requirements for a nominal 250 °F cure epoxy preimpregnated carbon fiber plain weave fabric product. The prepreg is a plain weave fabric with 12K tows, a nominal fiber areal weight of 193 gsm, and nominal resin content of 42%.
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.
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:| Standard | Published | Revision | Status |
|---|---|---|---|
| AMS3914 | 2012-09-14 | Latest |
- SAE AMS 3914
- Aerospace
- Composite materials
- Fabrics
- Fibers
- Glass
- Lightweight materials
- Resins
- Materials properties