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现行 SAE AMS6891/2
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Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 40, Class 1, Grade 196, Style 6K-PW 航空航天用350°F(177°C)固化的碳纤维和玻璃纤维环氧树脂/预浸料产品:40型 1级 196级 6K-PW型
发布日期: 2020-12-29
本规范旨在采购QPL上列出的材料;因此,未提供限定或等效阈值。打算进行新材料鉴定或等效程序的用户必须参考本基本规范的质量保证章节AMS6891。
The intent of this specification is for the procurement of the material listed on the QPL; therefore, no qualification or equivalency threshold values are provided. Users that intend to conduct a new material qualification or equivalency program must refer to the Quality Assurance section of this base specification, AMS6891.
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现行
SAE AMS6891
Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications
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SAE AMS6891/1
Carbon Fiber and Fiberglass Epoxy Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 35, Class 1, Grade 191
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现行
SAE AMS6891/4
Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 42, Class 4, Grade 48, Style 108
航空航天用350华氏度(177摄氏度)固化的碳纤维和玻璃纤维环氧树脂/预浸料产品:42型 4级 48级 108型
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SAE AMS6891/3
Carbon Fiber and Fiberglass Epoxy/Prepreg Products with 350 °F (177 °C) Cure for Aerospace Applications: Type 34, Class 4, Grade 294, Style 7781
航空航天用350华氏度(177摄氏度)固化的碳纤维和玻璃纤维环氧树脂/预浸料产品:34型 4级 294级 7781型
2021-03-10
现行
MIL MIL-T-29586/1 Notice 1-Cancellation
THERMOSETTING POLYMER (EPOXY) MATRIX, 350 DEG. F(177 DEG. C) CURE, INTERMEDIATE MODULUS CARBON FIBER REINFORCED PREPREG TAPE, (WIDTHS UP TO 60 INCHES) (NO S/S DOCUMENT)
热固性聚合物(环氧树脂)基体 350华氏度(177摄氏度)固化 中等模量碳纤维增强预浸带 (宽度可达60英寸)(无文件)
1996-10-09
现行
MIL MIL-T-29586/1
THERMOSETTING POLYMER (EPOXY) MATRIX, 350 DEG. F(177 DEG. C) CURE, INTERMEDIATE MODULUS CARBON FIBER REINFORCED PREPREG TAPE, (WIDTHS UP TO 60 INCHES) (NO S/S DOCUMENT)
热固性聚合物(环氧树脂)基体 350华氏度(177摄氏度)固化 中等模量碳纤维增强预浸带 (宽度可达60英寸)(无S/S文件)
1991-04-30