V10 航空、航天材料基础标准 标准查询与下载

SAE AS7101B-2002 美国国家航空航天和国防承包商认证计划(NADCAP)一般要求,主要针对材料测试实验室认可计划

1.1 This standard establishes the minimum requirements for materials testing laboratories (MTL)accredited by NADCAP. The following test methods and processes for metallic material systemsare covered in this standard.a. Chemical Testingb. Mechanical Testingc. Metallography and Microhardnessd. Hardnesse. Corrosionf. Mechanical Testing Specimen Preparationg. Differential Thermal Analysish. Heat Treatingi. X-Ray Diffractionj. Fastener Testing

NATIONAL AEROSPACE AND DEFENSE CONTRACTORS ACCREDITATION PROGRAM (NADCAP) GENERAL REQUIREMENTS FOR MATERIALS TEST LABORATORY ACCREDITATION PROGRAM

NAVY MIL-S-8512 D REINST NOTICE 2-2002 用于海军MIL-S-008512 C特殊航空支援设备一般规格的设计

MIL-S-8512D(2), dated 14 March 1980, is hereby reinstated and may be used for acquisition

SUPPORT EQUIPMENT, AERONAUTICAL, SPECIAL, GENERAL SPECIFICATION FOR THE DESIGN OF [Use In Lieu Of: NAVY MIL-S-008512 C]

SAE AMS3044E-2002 干粉湿法荧光磁性颗粒

1.1 Form:This specification covers fluorescent magnetic particles in the form of a dry powder.1.2 Application:These particles have been used typically as the inspection medium in wet, fluorescent magneticparticle inspection system as defined in ASTM E 1444 using either an oil or conditioned-watervehicle, but usage is not limited to such application.1.3 Safety - Hazardous Materials:While the materials, methods, applications, and processes described or referenced in thisspecification may involve the use of hazardous materials, this specification does not address thehazards which may be involved in such use. It is the sole responsibility of the user to ensurefamiliarity with the safe and proper use of any hazardous materials and to take necessaryprecautionary measures to ensure the health and safety of all personnel involved.

Magnetic Particles, Fluorescent, Wet Method, Dry Powder

SAE AS81807-2002 飞机地面支持设备标记和其他飞行航线车辆倒退反射材料;FSC 1730过程

Marking of Aircraft Ground Support Equipment and Other Flight Line Vehicles with Retro-Reflective Materials; Process For FSC 1730;This specification prescribes general requirments for marking of aircraft ground support equipment and other vehicles(i.e, runway sweepers,firetrucks,refulers,etc.),used on or near the flight line area with retro-reflective matertals.

Marking of Aircraft Ground Support Equipment and Other Flight Line Vehicles with Retro-Reflective Materials; Process For FSC 1730

SAE AMS1452B-2002 一般用途飞机用消毒剂

This specification covers a concentrated liquid primarily for disinfecting lavatories and galleys of passenger aircraft.

Disinfectant, Aircraft, General Purpose

NAVY QPL-24453-14-2002 水溶性油腐蚀抑制剂

This list has been prepared for use by or for the Government in the acquisition of products covered by the subject specification and such listing of a product is not intended to and does not connote endorsement of the product by the Department of Defense.

INHIBITOR, CORROSION, SOLUBLE-OIL

ARMY MIL-DTL-382 D VALID NOTICE 1-2002 镁粉-弹药用

MIL-DTL-382D, dated 20 January 1998, has been reviewed and determined to be valid for use in acquisition

MAGNESIUM POWDER - FOR USE IN AMMUNITION

ASTM F942-02(2008) 航天透明外壳用的夹层材料试验方法选择的标准指南

This guide is intended for use by material suppliers, aircraft transparent enclosure fabricators, airframe manufacturers, government agencies, and others that may become involved in the testing of transparent interlayer materials. These test methods provide data on both individual interlayer materials and material combinations commonly used in the fabrication of aerospace transparent enclosures and provide a means of evaluating the performance of one interlayer material against another. Primary characteristics and their long-term stability are critical to the performance of an interlayer material. Basic tests define the as-manufactured material characteristics of the interlayer material. Ageing procedures provide for representative exposure to environments that may induce changes in material characteristics. Tests performed before and after ageing exposure provide a means of estimating the potential useable life-span of an interlayer material or to compare the durability of one interlayer material with another. When employing these test methods for the comparison of interlayer materials after exposure to selected environmental conditions, the user shall be aware that many factors influencing degradation due to weathering vary from one location and exposure period to another location and exposure period. For direct weathering comparisons, the interlayer materials to be compared shall be subjected to the exposure and have the tests performed at the same time. It is emphasized that the test values obtained under these simultaneously applied conditions are for comparative use and their use as design characteristics shall be made with caution. The test methods listed include those considered critical to the performance of aircraft transparent enclosures. The user is advised to use the latest revision of any test method.1.1 This guide summarizes the standard test methods available for determining physical and mechanical characteristics of interlayer materials used in multi-ply aerospace transparent enclosures. 1.2 Interlayer materials are used to laminate glass-to-glass, glass-to-plastic, and plastic-to-plastic. Interlayer materials are basically transparent adhesives with high-quality optical properties. They can also serve as an energy absorbing medium, a fail-safe membrane to contain cockpit pressure and to prevent entry of impact debris; a strain insulator to accommodate different thermal expansion rates of members being laminated and as an adherent to prevent spalling of inner surface ply material fragments. The relative importance of an interlayer characteristic will be a function of the prime use it serves in its particular application. 1.3 This guide, as a summary of various methods in Section 2, is intended to facilitate the selection of tests that can be applied to interlayer materials. 1.4 The test methods listed are for use in determining basic design characteristics and in assuring lot-to-lot uniformity of the materials being tested except as noted in 3.3. 1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and heal practices and determine the applicability of regulatory limitations prior to use.

Standard Guide for Selection of Test Methods for Interlayer Materials for Aerospace Transparent Enclosures

ASTM F942-02 航空航天透明外壳用的夹层材料试验方法选择的标准指南

1.1 This guide summarizes the standard test methods available for determining physical and mechanical characteristics of interlayer materials used in multi-ply aerospace transparent enclosures.1.2 Interlayer materials are used to laminate glass-to-glass, glass-to-plastic, and plastic-to-plastic. Interlayer materials are basically transparent adhesives with high-quality optical properties. They can also serve as an energy absorbing medium, a fail-safe membrane to contain cockpit pressure and to prevent entry of impact debris; a strain insulator to accommodate different thermal expansion rates of members being laminated and as an adherent to prevent spalling of inner surface ply material fragments. The relative importance of an interlayer characteristic will be a function of the prime use it serves in its particular application.1.3 This guide, as a summary of various methods in Section 2, is intended to facilitate the selection of tests that can be applied to interlayer materials.1.4 The test methods listed are for use in determining basic design characteristics and in assuring lot-to-lot uniformity of the materials being tested except as noted in 3.3.1.5 This standard does not purport to address all of the safety concerns, if any, associated with its use. It is the responsibility of the user of this standard to establish appropriate safety and heal practices and determine the applicability of regulatory limitations prior to use.

Standard Guide for Selection of Test Methods for Interlayer Materials for Aerospace Transparent Enclosures

ARMY JAN-D-709 VALID NOTICE 2-2002 邻苯二甲酸二甲酯(用于炸药)

JAN-D-709 remains inactive for new design, however, the document is valid for use.

DIMETHYLPHTHALATE (FOR USE IN EXPLOSIVES)

SAE AMS3168-2001 用于应用密封性化合物之前清洗的含水清洁剂

This specification covers liquid aqueous cleaners. These aqueous cleaners have been used typically for cleaning aircraft primary and secondary structural surfaces prior to application of adhesion promoters and/or sealing materials, but usage is not limited to such applications.

Aqueous Cleaners for Cleaning Prior to Application of Sealing Compounds

DLA A-A-52040 VALID NOTICE 1-2001 (袖珍)航空摄影分析透镜立体显微镜

A-A-52040, dated 6 January 1992, has been reviewed and determined to be valid for use in acquistion.

STEREOSCOPES, LENS, AERIAL PHOTOGRAPH INTERPRETATION (POCKET)

AECMA PREN 4179-2001 航空航天系列.非破坏性测试

This "Aerospace Series" Prestandard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on green paper for the needs of AECMAMembers. It has been technically approved by the experts of the concerned Technical Committee following comment by the Member countries.

Aerospace Series Qualification and Approval of Personnel for Non-Destructive Testing Edition P 2; Supersedes Edition P 1: January 1995; Replaced by EN 4179

AECMA PREN 4364-2001 航空系列 铸件丙烯酸道具.P1版

This "Aerospace series" Standard has been drawn up under the responsibility of AECMA (The European Association of Aerospace Industries). It is published on yell0 w paper in three equivalent versions (English, French, German). It will be submitted as a draft European Standard to CEN (European Committee for Standardization) for formal vote.

Aerospace Series Cast Acrylic Properties Edition P 1

NAVY MIL-DTL-82965 B-2001 高能硝胺枪械推进剂

The HPLC conditions may require alterations to achieve the desired resolution. This largely depends on the individual column.

PROPELLANT, GUN, HIGH ENERGY NITRAMINE

ARMY MIL-PRF-71208-2001 M995型5.56mm穿甲炮弹

This specification covers the Cartridge,5.56mm, Armor Piercing, M995

CARTRIDGE, 5.56MM, ARMOR PIERCING, M995

SAE AMS-T-81533-2001 禁止使用三氯乙烷1,1,1,(三氯乙烷)的蒸气除油.代替MIL-T-81533

This specification has been declared "CANCELLED" by the Aerospace Materials Division, SAE, as of April, 2007. By this action, this document will remain listed in the Numerical Section of the Index of Aerospace Material Specifications, indicating that it has been "CANCELLED". This specification covers the requirements of inhibited 1, 1, 1 trichloroethane for vapor degreasing.

Trichloroethane 1, 1, 1, (Methyl Chloroform) Inhibited, Vapor Degreasing Replaces MIL-T-81533

SAE AMS2435F-2001 碳化钨钴涂层的爆震燃烧过程

This specification covers the engineering requirements for applying tungsten carbide/cobalt coatingsto metal parts by the detonation process and the properties of such coatings.

Coating, Tungsten Carbide-Cobalt Detonation Process

ARMY MIL-F-71149 (7)-2001 M779型引信引爆点与签署炮弹

MIL-S-747WA(USAF), dated W9 december 1975, has been reviewed and determined to be current.

FUZE, POINT DETONATING, PRACTICE, M779 WITH PYROTECHNIC SIGNATURE CARTRIDGE

SAE AMS3165E-2001 石油芳香族溶剂

1.1 Form:This specification covers a petroleum-base liquid solvent.1.2 Application:This solvent has been used typically for use as a paint thinner and as a solvent cleaner to remove oiland oil-bonded contaminants from metal surfaces.1.3 Safety - Hazardous Materials:While the materials, methods, applications, and processes described or referenced in thisspecification may involve the use of hazardous materials, this specification does not address thehazards which may be involved in such use. It is the sole responsibility of the user to ensurefamiliarity with the safe and proper use of any hazardous materials and to take necessaryprecautionary measures to ensure the health and safety of all personnel involved.

Solvent, Petroleum Aromatic