V10 航空、航天材料基础标准 标准查询与下载

DLA MIL-DTL-7989 C-2006 通用技术条件航空灯光传输盖

This specification is approved for use by all Departments and Agencies of the Department of Defense.

COVERS, LIGHT-TRANSMITTING, FOR AERONAUTICAL LIGHTS, GENERAL SPECIFICATION FOR

ARMY MIL-DTL-60426 B (1)-2006 M54A1型起爆弹

The documents listed in this section are specified in sections 3 and 4 of this specification. This section does not include documents in other sections of this specification or recommended for additional information or as examples. While every effort has been made to assure the completeness of this list, document users are cautioned that they must meet all requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed.

BURSTER, PROJECTILE-M54A1

ARMY MIL-DTL-60585 B (1)-2006 M1E1型实心起爆弹

The documents listed in this section are needed to meet the requirements specified in sections 3 and 4 of this specification. This section does not include documents in other sections of this specification or recommended for additional information or as examples. While every effort has been made to assure the completeness of this list, document users are cautioned that they must meet all requirements documents cited in sections 3 and 4 of this specification, whether or not they are listed.

CASE, PROJECTILE BURSTER - ASSEMBLY, M1E1

AIR FORCE MIL-DTL-25988 C-2006 柔性管液压传动系统飞行器燃料和油阻润滑油燃料氟橡胶

This specification covers oil- and fuel-resistant fluorosilicone elastomer rubber sheets, strips, molded parts, and extruded shapes for aeronautical and aerospace applications.

RUBBER, FLUOROSILICONE ELASTOMER, OIL-AND FUEL-RESISTANT, SHEETS, STRIPS, MOLDED PARTS, AND EXTRUDED SHAPES

SAE AMS2759/10A-2006 由氮化电位控制自动化气体氮化

This specification establishes requirements and procedures for generating nitrided surfaces on steel parts using a process controlled by the nitriding potential. The nitriding process described herein is used typically to produce a nitride case on carbon and alloy steels, tool steels, nitriding steels, corrosion resistant steels and other ferrous alloys. Applicable, allowance should be made for growth.

Automated Gaseous Nitriding Controlled by Nitriding Potential

ARINC 817-2006 航空电子设备数字视频母线低数据率

AVIONICS DIGITAL VIDEO BUS LOW-DATA RATE - UNCOMPRESSED

AVIONICS DIGITAL VIDEO BUS LOW-DATA RATE - UNCOMPRESSED

BS ISO 14624-5:2006 航天系统.材料的安全和兼容性.航空航天推进器的系统/组件材料的活性测定

This part of ISO 14624 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid. This part of ISO 14624 may be used to determine the reactivity of system and component materials with aerospace fluids. It is applicable for determining interactive reactions between propellants and materials used in the design, construction, and operation of propellant storage, transfer, and flight systems. While this procedure is an excellent quick screen test for long-term propellant compatibility, it is semi-qualitative, and (if exposures exceed 12 months) long-term tests need to be used to quantify degradation as a function of time under use conditions.

Space systems - Safety and compatibility of materials - Determination of reactivity of system/component materials with aerospace propellants

BS ISO 14624-6:2006 航天系统.材料的安全和兼容性.航空航天流体的加工材料的活性测定

This part of ISO 14624 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid. This part of ISO 14624 can be used to determine the reactivity of processing materials with aerospace fluids either through intent or casual exposure. It provides a means to determine the effects of minor amounts of fluids, such as a splash or spill, on materials used in ground support processing operations.

Space systems - Safety and compatibility of materials - Determination of reactivity of processing materials with aerospace fluids

BS ISO 14624-7:2006 航天系统.材料的安全和兼容性.航空航天流体材料穿透率和渗透性的测定

This part of ISO 14624 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid. This part of ISO 14624 can be used to determine the reactivity of materials with aerospace fluids. It provides a means to determine the effects of minor amounts of aerospace fluids, such as in a splash or spill, on materials used in ground support processing operations, and in the selection of personal safety equipment.

Space systems - Safety and compatibility of materials - Determination of permeability and penetration of materials to aerospace fluids

ARMY MIL-DTL-70793 A-2006 M940型20MM多功能微量自毁弹

This specification covers the Cartridge, 20MM: Multipurpose, Trace Self Destruct, M940, for applications in different Air Defense systems. Certain requirements for the ammunition are based on the end system application

CARTRIDGE, 20MM: MULTIPURPOSE, TRACE SELF-DESTRUCT, M940

ARMY MIL-DTL-46540 C-2006 M103型弹壳

This specification covers the Case, Cartridge: 20MM, M103 for use with 20 millimeter ammunition(see 6.1).

CASE, CARTRIDGE: 20MM, M103

DLA A-A-20087 C-2006 酱油

This CID covers soy sauce packed in commercially acceptable containers, suitable for use by Federal, State, local governments, and other interested parties; and as a component of operational rations.

SOY SAUCE

ISO 14624-5:2006 航天系统.材料的安全和兼容性.第5部分:航空航天推进器的系统/组件材料的活性测定

This part of ISO 14624 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid. This part of ISO 14624 may be used to determine the reactivity of system and component materials with aerospace fluids. It is applicable for determining interactive reactions between propellants and materials used in the design, construction, and operation of propellant storage, transfer, and flight systems. While this procedure is an excellent quick screen test for long-term propellant compatibility, it is semi-qualitative, and (if exposures exceed 12 months) long-term tests need to be used to quantify degradation as a function of time under use conditions.

Space systems - Safety and compatibility of materials - Part 5: Determination of reactivity of system/component materials with aerospace propellants

DLA O-M-232 L-2006 甲醇

This specification covers three grades and four unit quantities of methanol.

METHANOL (METHYL ALCOHOL)

ASTM E1216-06 用胶带提取法对表面微粒子污染取样的标准规程

The tape lift provides a rapid and simple technique for removing particles from a surface and determining their number and size distribution. By using statistically determined sample size and locations, an estimate of the surface cleanliness level of large areas can be made. The user shall define the sampling plan. The sampling plan shall consider the importance of surface geometry and surface orientation to gas flow, gravity, obstructions, and previous history of hardware. These factors influence particle fallout and entrapment of particles on the surface. The geometry of joints, recessed areas, fasteners, and the correspondence of particle-count data to area can be maintained. The selection of tape and the verification of its effect on the cleanliness of the hardware is very important. The tape adhesive should have sufficient cohesion to avoid transfer of the adhesive to the surface under test. The impact of adhesive transfer should be evaluated by laboratory testing before using the tape on the hardware. Since potential for adhesive transfer exists, cleaning to remove any adhesive might be required. In addition, the tape should have low outgassing characteristics, and as a minimum, it should meet the requirements of less than 1.0 % total mass loss (TML) and 0.1 % collected volatile condensable materials (CVCM), as measured by Test Method E 595. Care should be exercised in deciding which surfaces should be tested by this practice. The tape can remove marginally adhering paint and coatings. Optical surfaces should not be tested until verification has been made that the surface coating will not be damaged. Rough surface finishes result in low removal efficiencies. Surface finishes up to approximately 3.20 μm (125 μin.) have been tested and found to give satisfactory results. This practice has been tested only on surfaces at room temperature. Evaluation of temperature effects must be conducted prior to using the test on surfaces other than room temperature. Only personnel experienced in microscopic particle-counting techniques should be used to count and size the particles.1.1 This practice covers procedures for sampling surfaces to determine the presence of particulate contamination, 5 m and larger. The practice consists of the application of a pressure-sensitive tape to the surface followed by the removal of particulate contamination with the removal of the tape. The tape with the adhering particles is then mounted on counting slides. Counting and measuring of particles is done by standard techniques.1.2 This practice describes the materials and equipment required to perform sampling of surfaces for particle counting and sizing.1.3 The criteria for acceptance or rejection of a part for conformance to surface cleanliness level requirements shall be determined by the user and are not included in this practice.1.4 This practice is for use on surfaces that are not damaged by the application of adhesive tape. The use of this practice on any surface of any material not previously tested or for which the susceptibility to damage is unknown is not recommended. In general, metals, metal plating, and oxide coatings will not be damaged. Application to painted, vapor deposited, and optical coatings should be evaluated before implementing this test.1.5 This practice provides three methods to evaluate tape lift tests, as follows:SectionsPractice A-This method uses light transmitted through the tapeand tape adhesive to detect particles that adhere to it.4 to 6Practice B-This method uses light transmitted through the tapeadhesive after bonding to a base micr......

Standard Practice for Sampling for Particulate Contamination by Tape Lift

ARMY MIL-C-70796 (1) CONT. DIST.-2006 M20A1型105MM榴弹炮.加农炮

This commercial item description covers brown kraft paper used for general wrapping applications.

CANNON, 105MM HOWITZER: M20A1

ARMY MIL-DTL-60945 D-2006 M385A1型40MM发射弹.练习弹

This specification covers the requirements,examinations and tests for the Cartridge, 40MM - Projectile Assembly, Practice, M385A1.

CARTRIDGE, 40MM - PROJECTILE ASSEMBLY, PRACTICE, M385A1

QJ 3254-2005 航天用纤维增强聚氨酯泡沫塑料规范

本规范规定了航天用纤维增强聚氨酯泡沫塑料产品（以下简称产品）的要求、质量保证规定和交货准备等内容。 本规范适用于以短切玻璃纤维作增强体，聚醚多元醇与多异氰酯为主要原材料反应制得的纤维增强硬质聚氨酯泡沫塑料的板材和异型产品。

Specification for fiber reinforced polyurethane foams plastics for space

DLA A-A-59775-2005 滴油盘

The General Services Administration has authorized the use of this commercial item description as a replacement for Military Specifications MIL-V-16720E and MIL-V-16721D which are cancelled.

OIL PAN, DRIP

DLA A-A-59304 VALID NOTICE 1-2005 过氧化甲乙酮(催化剂) [代替:DLA MIL-P-87938 CANC 通告 1,DLA MIL-P-87938]

The activities above were interested in this document as of the date of this document. Since organizations and responsibilities can change, you should verify the currency of the information above using the ASSIST Online database at http://assist.daps.dla.mil

METHYL ETHYL KETONE PEROXIDE (CATALYST) [Superseded: DLA MIL-P-87938 CANC NOTICE 1, DLA MIL-P-87938]