標準號：SAE AMS 3914-2012
中文標準名稱：**復合材料半固化片.名義250℉硬化.12K拖碳纖維和環氧樹脂平紋織物
英文標準名稱：Advanced Composites Prepreg - Nominal 250 °F Cure - 12K Tow Carbon Fiber and Epoxy Resin, Plain Weave Fabric
標準類型：V13
發布日期：2012/9/18 12:00:00
實施日期：1999/12/31 12:00:00
中國標準分類號：V13
國際標準分類號：49.025.40
引用標準：ASTM D 792-2008;ASTM D 2344-1984;ASTM D 2734-2009;ASTM D 3039-1976;ASTM D 3171-2011;ASTM D 3530-1976;ASTM D 3532-1999;ASTM D 5379;ASTM E 4-2010;ASTM E 168-2006;ASTM E 1252-1998;DOT/FAA/AR-03/19;DOT/FAA/AR-06/10;MIL-HDBK-17;SACMA SRM 1R-94;SACMA SRM 18R-94
適用范圍：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.