V10 航空、航天材料基础标准 标准查询与下载

SAE AMS2430N-2008 自动喷丸加工处理

1.1 FormThis specification covers the engineering requirements for automatic peening of surfaces of parts by impingement of metallic shot, glass beads, or ceramic shot.1.2 ApplicationTo induce residual compressive stress in surface layers of parts, thereby increasing fatigue strength and resistance to stress-corrosion cracking but usage is not limited to such applications.

Shot Peening, Automatic

ASTM F1111-08b 用飞行器维护化学膜法测定低脆化镉板防腐蚀性的标准试验方法

The data generated by this test method shall be used to determine whether low embrittling cadmium plated parts are liable to be corroded or damaged by application of the test material during routine maintenance operations.1.1 This test method is intended as a means of determining the corrosive effects of aircraft maintenance chemicals on low-embrittling cadmium plating used on aircraft high-strength steel, under conditions of total immersion by quantitative measurements of weight change. 1.2 This standard may involve hazardous materials, operations, and equipment. 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 health practices and determine the applicability of regulatory limitations prior to use. For specific hazard statements see Section 6, 4.1.

Standard Test Method for Corrosion of Low-Embrittling Cadmium Plate by Aircraft Maintenance Chemicals

ARMY MIL-DTL-248 D (1)-2007 三硝基甲苯(TNT)

Trinitrotoluene(TNT). TNT covered by this specification is a high explosive intended for use in ammunition(see 6.1).

TRINITROTOLUENE (TNT)

DLA QPL-87218-5-2007 航天器控制装甲电缆

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.

CABLE, LOCKCLAD, FOR AIRCRAFT CONTROL

ARMY MIL-DTL-48623 A-2007 M1A1型50口径空包弹

This specification covers the requirements and verification methods for the Cartridge, Blank, Caliber.50, M1A1.

DETAIL SPECIFICATION CARTRIDGE, CALIBER.50, BLANK, M1A1

ARMY MIL-DTL-10190 E-2007 M33型50口径枪弹的普通弹

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

CARTRIDGE, CALIBER .50, BALL, M33

ARMY MIL-DTL-1318 C-2007 M17型50口径枪弹的示踪剂

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

CARTRIDGE, CALIBER .50, TRACER, M17

GJB 5989-2007 飞机座舱隔热隔音材料的包覆层规范

本规范规定了飞机座舱隔热隔音材料的包覆层的要求、质量保证规定、交货准备等。 本规范适用于飞机座舱隔热隔音材料的包覆层。

Specification for complex material for heat and sound insulation in aircraft cabin

ARMY MIL-D-60254 A REINST NOTICE 2-2007 M232型5.56MM惰性装练习弹

MIL-D-60254A(AR), dated 12 August 1966 with Amendment 2, is hereby reinstated and may be used for acquisition.

DUMMY CARTRIDGE, 5.56MM, M232, INERT LOADED

DLA A-A-52040 VALID NOTICE 2-2007 (袖珍)航空摄影分析透镜立体显微镜

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 assist.daps.dla.mil.

STEREOSCOPES, LENS, AERIAL PHOTOGRAPH INTERPRETATION (POCKET)

ARMY MIL-DTL-70953 B CONT. DIST.-2007 M119A1/A2型105MM轻工榴弹炮的反冲机制缓冲区

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

BUFFER, RECOIL MECHANISM ASSEMBLY, M119A1/A2 HOWITZER, LIGHT, TOWED: 105MM

ARMY MIL-DTL-71172 B(1) CONT. DIST.-2007 M119A1/A2型105MM榴弹炮的轻拖曳回热式热交换器

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

CYLINDER, RECUPERATOR, RECOIL, M119A1/A2 HOWITZER LIGHT, TOWED: 105MM

ARMY QPL-11891-25-2007 车载具有弹性的田径鞋套.田径鞋集会.田径鞋垫和田径鞋衬套

This list has been prepared for use by or for the Government in the actheof 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. All products listed herein have been qualified under the requirements for the product as specified in the latest effective issue of the applicable specification. This list is subject to change without notice; revision or amendment of this list will be issued as necessary. The listing of a product does not release or otherwise affect the obligation of the manufacturer to comply with the specification requirements.

TRACK SHOE SETS, TRACK SHOE ASSEMBLIES, TRACK SHOE PADS AND TRACK SHOE BUSHINGS, VEHICULAR: ELASTOMERIZED

ASTM E1997-07 航天器材料的选择用标准实施规程

This practice is a guideline for proper materials and process selection and application. The specific application of these guidelines must take into account contractual agreements, functional performance requirements for particular programs and missions, and the actual environments and exposures anticipated for each material and the equipment in which the materials are used. Guidelines are not replacements for careful and informed engineering judgment and evaluations and all possible performance and design constraints and requirements cannot be foreseen. This practice is limited to unmanned systems and unmanned or external portions of manned systems, such as the Space Station. Generally, it is applicable to systems in low earth orbit, synchronous orbit, and interplanetary missions. Although many of the suggestions and cautions are applicable to both unmanned and manned spacecraft, manned systems have additional constraints and requirements for crew safety which may not be addressed adequately in unmanned designs. Because of the added constraints and concerns for human-rated systems, these systems are not addressed in this practice.1.1 The purpose of this practice is to aid engineers, designers, quality and reliability control engineers, materials specialists, and systems designers in the selection and control of materials and processes for spacecraft, external portion of manned systems, or man-tended systems. Spacecraft systems are very different from most other applications. Space environments are very different from terrestrial environments and can dramatically alter the performance and survivability of many materials. Reliability, long life, and inability to repair defective systems (or high cost and difficultly of repairs for manned applications) are characteristic of space applications. This practice also is intended to identify materials processes or applications that may result in degraded or unsatisfactory performance of systems, subsystems, or components. Examples of successful and unsuccessful materials selections and uses are given in the appendices.

Standard Practice for the Selection of Spacecraft Materials

ASTM E595-07 真空环境中放气引起的总质量损失及收集的挥发性可凝结物的测定用标准试验方法

This test method evaluates, under carefully controlled conditions, the changes in the mass of a test specimen on exposure under vacuum to a temperature of 125°C and the mass of those products that leave the specimen and condense on a collector at a temperature of 25°C. The 24 h test time does not represent actual outgassing from years of operation, so a higher test temperature shorter time was selected to allow material comparisons with no intent to predict actual outgassing in service. The test temperature of 125°C was assumed to be significantly above the expected operating temperature in service. If expected operating temperatures exceed 65 to 70°C the test temperature should be increased. It is suggested that test temperature be at least 30°C higher than expected maximum service temperature in order to provide material comparisons for TML and CVCM. Comparisons of material outgassing properties are valid at 125°C sample temperature and 25°C collector temperature only. Samples tested at other temperatures may be compared only with other materials which were tested at that same temperature. The measurements of the collected volatile condensable material are also comparable and valid only for similar collector geometry and surfaces at 25°C. Samples have been tested at sample temperatures from 50 to 400°C and at collector temperatures from 1 to 30°C by this test technique. Data taken at nonstandard conditions must be clearly identified and should not be compared with samples tested at 125°C sample temperature and 25°C collector temperature. The simulation of the vacuum of space in this test method does not require that the pressure be as low as that encountered in interplanetary flight (for example, 10−12 Pa (10−14 torr)). It is sufficient that the pressure be low enough that the mean free path of gas molecules be long in comparison to chamber dimensions. This method of screening materials is considered a conservative one because maximum operating temperatures in service are assumed not to exceed 50 to 60°C for most applications. It is possible that a few materials will have acceptable properties at the intended use temperature but will be eliminated because their properties are not satisfactory at the test temperature of 125°C. Also, materials that condense only below 25°C are not detected. The user may designate additional tests to qualify materials for a specific application. The determinations of TML and WVR are affected by the capacity of the material to gain or lose water vapor. Therefore, the weighings must be accomplished under controlled conditions of 23°C and 50 % relative humidity. Alternatively, all specimens may be put into open glass vials during the 24-h temperature and humidity conditioning. The vials must be capped before removal from the conditioning chamber. Each specimen must be weighed within 2 min after opening the vial to minimize the loss or absorption of water vapor while exposed to an uncontrolled humidity environment. While control of humidity is not necessary at this point, the temperature for the weighing should be controlled at 23°C, the same temperature prescribed for t......

Standard Test Method for Total Mass Loss and Collected Volatile Condensable Materials from Outgassing in a Vacuum Environment

SAE AMS2759/12A-2007 电压自动控制的气体渗碳剂

This specification covers the requirements for producing a continuous compound layer with controlled phase composition by means of a gaseous process, automatically controlled to maintain set values of the nitriding and carburizing potentials that determine properties of the nitrocarburized surface. Automatic control is intended to ensure repeatability of nitrogen and carbon content of the compound layer which establishes properties such as wear and corrosion resistance, ductility and fatigue strength.

Gaseous Nitrocarburizing, Automatically Controlled by Potentials

GJB 5907-2006 导弹用多晶硫化锌整流罩材料规范

本规范规定了导弹用热压多晶硫化锌整流罩材料的要求、质量保证规定、交货准备等。 本规范适用于导弹用多晶硫化锌整流罩材料。

Specification for polycrystal zinc sulfide dome materials for missiles

HB 7802-2006 BOM通用要求

本标准规定了BOM分类与构成、构造与转换、使用与管理等要求。 本标准适用于飞机产品的研制和生产过程，其它航空产品可参照使用。

General requirements for BOM

ARINC 818-2006 航空电子设备数字视频母线高数据率2007年3月8号

AVIONICS DIGITAL VIDEO BUS HIGH DATA RATE Incorporates Errata: March 8, 2007

AVIONICS DIGITAL VIDEO BUS HIGH DATA RATE Incorporates Errata: March 8, 2007

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