V04 基础标准与通用方法 标准查询与下载

ISO/TR 23462:2007 航天系统.航天规划管理框架的定义指南

This Technical Report provides a framework within which an organization can establish the basis for the development of programme/project management specifications and plans when undertaking the execution of a specific programme/project. It enables the programme/project manager to establish the criteria for programme/project success and to secure the organization’s commitment to the programme/project manager’s management approach for the overall programme/project and its constituent elements. It includes guidelines leading to the establishment of a programme/project management framework, and identification of practices to be applied. Following these guidelines also results in traceability of the considerations and decisions on why and how the programme/project is conducted according to its specific characteristics. This Technical Report provides a holistic approach for programme/project managers to apply their organization's programme/project management practices when defining the management framework for programme/project planning. It is based on a systematic method of defining the programme/project objectives and success criteria, identifying and elaborating the specific characteristics of their programme/project, specifying the management elements needed, establishing and agreeing the management approaches to be implemented, compiling these into a programme/project management framework document. The guidelines in this Technical Report are applicable to any organization undertaking the execution of space programmes/projects.

Space systems - Guidelines to define the management framework for a space project

DLA QPL-87161-9-2007 飞行器应用非灵活钢丝索

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. 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 the contractor from compliance with the specification requirements.

WIRE STRAND, NONFLEXIBLE, FOR AIRCRAFT APPLICATION

DLA QPL-9398-15-2007 飞行器高温双极转数表生成器

MIL-G-9398 was made "Inactive for New Design" with no superseding specification on 14 September 1998.

GENERATOR, TACHOMETER, TWO-POLE, HIGH TEMPERATURE, AIRCRAFT

DLA QPL-83420-15-2007 飞行器控制灵活钢绳的常规

his 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. 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 the supplier from compliance with the specification requirements.

WIRE ROPE, FLEXIBLE, FOR AIRCRAFT CONTROL, GENERAL SPECIFICATION FOR

DIN EN 4408-003:2007 航空航天系列.技术图.复合材料制造部件的表示法.第3部分:包括芯材的部件

This standard specifies the rules for the representation of parts including core materials as well as the information to be indicated in technical drawings. It applies to aerospace structures using core materials. It shall be used together with EN 4408-001.

Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 3: Parts including core materials; German and English version EN 4408-003:2005

DIN EN 4408-001:2007 航空航天系列.技术图.复合材料制造部件的表示法.第1部分:一般要求

This standard specifies the general rules for the representation of parts made of composite materials,in technical drawings. It applies to aerospace structures using composites materials,and their applications when this standard is specified.

Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 1: General rules; German and English version EN 4408-001:2005

DIN EN 4408-002:2007 航空航天系列.技术图.复合材料制造部件的表示法.第2部分:层压部件

This standard specifies the rules for the representation of laminated parts as well as the information to be indicated in technical drawings. It applies to aerospace structures using laminated parts.It shall be used together with EN 4408-001.

Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 2: Laminated parts; German and English version EN 4408-002:2005

DIN EN 4408-005:2007 航空航天系列.技术图.复合材料制造部件的表示法.第5部分:缝隙

This standard specifies the representation of seams of composite materials as well as the information to be indicated in technical drawings. It is applicable to aerospace structures using items linked by seams in dry fabrics,prepregs,film,etc. It shall be used together with EN 4408-001.

Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 5: Seams; German and English version EN 4408-005:2005

DIN EN 4408-006:2007 航空航天系列.技术图.复合材料制造部件的表示法.第6部分:预先成型件

This standard specifies the rules for the representation of preforms of composite materials as well as the information to be indicated in the technical drawings. It is applicable to aerospace structures using preforms. It shall be used together with EN 4408-001.

Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 6: Preforms; German and English version EN 4408-006:2005

DIN EN 4408-004:2007 航空航天系列.技术图.复合材料制造部件的表示法.第4部分:缠绕产品

This standard specifies the rules for the representation of items in composite materials obtained by winding as well as the information to be indicated in technical drawings. It is applicable to aerospace structures using items in composite materials obtained by winding. It shall be used together with EN 4408-001.

Aerospace series - Technical drawings - Representation of parts made of composite materials - Part 4: Items obtained by winding; German and English version EN 4408-004:2005

NAVY A-A-59734 VALID NOTICE 1-2007 振动筘转速表

A-A-59734, dated 09 August 2002, has been reviewed and determined to be valid for use in acquisition.

TACHOMETER, VIBRATING REED

BS ISO 21348:2007 航天环境(天然和人造).太阳辐照度的测定过程

ISO 21348:2007 specifies the process for determining solar irradiances and is applicable to measurement sets, reference spectra, empirical models, theoretical models, and solar irradiance proxies or indices that provide solar irradiance products representing parts or all of the solar electromagnetic spectrum. Its purpose is to create a standard method for specifying all solar irradiances for use by space systems and materials users.

Space environment (natural and artificial). Process for determining solar irradiances

HB 9103-2007 关键特性的波动管理

1.1 目的 本标准通过充分策划以及对关键特性波动的有效管理来推动制造过程的改进。关键特性主要用于提高对零件特性的信心，这些特性的波动对最终产品的形成、装配、性能、使用寿命和可制造性具有重大 影响。 1.2 适用性 本标准主要针对新制零部件，也适用于在制零部件。本标准应在影响关键特性波动的所有生产过程使用。 本标准适用于部件及部件中所有层次的零件，包括铸件和锻件，并适用于负责实现产品设计特性的组织。各生产方及其供方应负责将本标准的适用版本的要求向下传递到实现设计特性的供方，并确保关键特性符合顾客要求。

Variation management of key characteristics

HB 9132-2007 用于零件标记的DATA MATRIX码的质量要求

本标准规定了航空行业内使用 DATA MATRIX 符号标记金属零件的有关质量和技术要求。ISO/IEC16022 规定了一般要求（数据字符编码、纠错规则、译码算法等）。除遵守ISO/IEC 16022 的有关规定外，使用 DATA MATRIX 符号的零件标记还需满足本标准的要求以确保电子识读符号的能力。 本标准包含下列标记过程：打点标记、激光标记、电化学蚀刻标记。如需要，将来可包括更多的标记过程。 本标准未规定有关编码方面的信息。 除非商业合同中另有规定，负责零件设计的公司应确定 DATA MATRIX 码标记的位置。符号位置应使各个方向都适宜识读。

Data matrix quality requirements for parts marking

GJB 2464A-2007 飞机透明件鸟撞试验方法

本标准规定了飞机透明件鸟撞试验方法。 本标准适用于各类飞机透明件及其支承结构的鸟撞试验。 飞机机翼、尾翼、雷达罩、发动机以及机车风挡玻璃等部件的鸟撞试验可参照执行。

Test method for bird impact of aircraft glazing materials

SAE AS5706-2007 延伸距离的AS5643/1 S400型铜介质接口特性用试验规划/试验程序

This document establishes test plans/procedures for the AS5643/1 Slash Sheet. The AS5643/1 Slash Sheet establishes guidelines for the use of IEEE-1394b as a data bus network in military and aerospace vehicles. It encompasses the data bus cable and its interface electronics for a system utilizing S400 over copper medium over extended lengths.

Test Plan/Procedure for AS5643/1 S400 Copper Media Interface Characteristics Over Extended Distances

SAE AMS2442A-2007 部件的磁性粒子验收标准

This specification establishes acceptance criteria for discontinuities revealed by magnetic particle inspection of parts made from wrought, ferromagnetic materials. These criteria are intended typically for, but not limited to, aerospace parts that require magnetic particle inspection following the completion of fabrication operations.

Magnetic Particle Acceptance Criteria for Parts

SAE AS9104/3-2007 航空航天审核员资格和培训课程要求

This document provides the minimum requirements (Body of Knowledge) for AQMS auditors who will participate in AQMS certification/registration activities, including the auditor authentication process and requirements for a training organization. It is applicable to auditors seeking formal approval to conduct audits of the AQMS in support of the IAQG, and those who manage the competency element of an AQMS audit program and/or training organizations.

Requirements for Aerospace Auditor Competency and Training Courses

DLA A-A-50203 A VALID NOTICE 2-2007 制图圆规

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.

COMPASS, DRAFTING, BEAM

DLA A-A-50204 A VALID NOTICE 2-2007 比例制图双脚规

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.

DIVIDER, DRAFTING, PROPORTIONAL