SAE AMS3961-2015
350°F 高压灭菌固化 低流动性增韧环氧树脂预浸料
350 °F Autoclave Cure@ Low Flow Toughened Epoxy Prepregs
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- 标准号
- SAE AMS3961-2015
- 发布
- 2015年
- 发布单位
- SAE - SAE International
- 当前最新
- SAE AMS3961-2015
- 适用范围
- The intent of this specification is for the procurement of the material listed on the QPL and@ therefore@ no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program shall refer to the Quality Assurance section of this base specification@ AMS3961. All material qualification and equivalency data has been archived and is available for review upon request. Contact the CMH-17 Secretariat (www.cmh17.org) for additional information. Purpose a. The purpose of this specification is to allow procurement of a defined material corresponding to the statistically derived material properties published in CMH-17. b. The materials qualified to this specification are designed specifically for vacuum-bag autoclave cure in accordance with 4.5. c. This specification is developed based on the material properties that are available publicly. The purchaser may specify additional requirements beyond those defined in this specification@ especially when the purchaser has generated additional material properties beyond those available publicly or when the application has other requirements. The additional requirements are subject to supplier review and approval. d. The use of this specification does not guarantee material or structural performance. Material users should be actively involved in evaluating material performance and quality including@ but not limited to@ performing regular purchaser quality control tests@ performing periodic equivalency/additional testing@ participating in material change management activities@ conducting statistical process control@ and conducting regular supplier audits. e. This material is intended for use in laminate applications with a service temperature range of -65 to 250 ?? f. This composite material may be used for the manufacture of primary and secondary aircraft structure.