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.
SAE AMS 3914-2012由美国机动车工程师协会 US-SAE 发布于 2012-09-18。
SAE AMS 3914-2012 在中国标准分类中归属于: V13 航空与航天用非金属材料,在国际标准分类中归属于: 49.025.40 橡胶和塑料。
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