SAE MAM2204 Tolerances, Metric, Aluminum Alloy Standard Structural Shapes (Cancelled Jul 1989, Superseded by ANSI H35.2(

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Product Code:SAE MAM2204
Title:Tolerances, Metric, Aluminum Alloy Standard Structural Shapes (Cancelled Jul 1989, Superseded by ANSI H35.2(M))
Issuing Committee:Ams D Nonferrous Alloys Committee
Scope: This specification covers established metric manufacturing tolerances applicable to aluminum alloy standard structural shapes ordered to metric dimensions. Standard structural shapes are shapes in certain standard alloys, tempers, sizes, and sections such as angles, channels, Tees, Zees, I-Beams, and H-Beams commonly used for structural purposes. These tolerances apply to all conditions, unless otherwise noted. This specification has been declared 'NONCURRENT' by the Aerospace Materials Division, SAE, as of September 1994. It is recommended, therefore, that this specification not be specified for new designs.
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基本信息
标准名称:太阳电池标定方法
英文名称:Test method for calibration of solar cells
中标分类: 航空、航天 >> 航天器及其附件 >> 航天器用能源设备
ICS分类: 航空器和航天器工程 >> 航空航天用电气设备与系统
替代情况:QJ 1017-1986
发布日期:2004-09-01
实施日期:2004-12-01
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页数:18页
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所属分类: 航空 航天 航天器及其附件 航天器用能源设备 航空器和航天器工程 航空航天用电气设备与系统
Product Code:SAE AMS3892/9
Title:Tow, Carbon Fiber, for Structural Composites, 500 (3447) Tensile Strength, 32 (221) Tensile Modulus
Issuing Committee:Ams P17 Composite Materials Committee
Scope:This specification covers one type of carbon fiber in the form of tow. Carbon tow with 500 ksi (3447 MPa) tensile strength and 32 Msi (221 GPa) tensile modulus for use in general purpose structural composites requiring high tensile strength and high modulus of elasticity in tension.