V04 基础标准与通用方法 标准查询与下载

GJB 6776.5-2009 空间目标测轨编目方法 第5部分：轨道内容与格式

本部分规定了空间目标测轨编目中编目轨道的内容与格式。 本部分适用于空间目标测轨编目轨道的数据交换与发布。

Method for space object detection and catalogue.Part 5:Content and format of orbital data

GJB 6671-2009 反舰导弹定型试验规程

本标准规定了反舰导弹定型试验、试验方案、实施程序、试验技术要求和试验结果评定原则。 本标准适用于反舰导弹定型试验基地试验（简称定型试验）。研制试验、部队试验和生产定型试验可参照使用。

Code for finalized test of anti-ship missile

GJB 6772-2009 导弹（运载火箭）外测应答机测试、对接要求

本标准规定了航天发射场导弹(运载火箭)外测应答机测试、对接的内容、方法及应遵循的一般技术要求。 本标准适用于航天发射场导弹(运载火箭)外测应答机测试、对接。

Unit checkout and matching test requirements for responder of missile(launch vehicle)tracking telemetry and command system

GJB 2235A-2009 试验弹药静态检测方法

本标准规定了炮弹、火箭弹和航空炸弹在试验过程中的静态检查和测量方法。 本标准适用于炮弹、火箭弹和航空炸弹设计定型和生产定型试验。鉴定、摸底和射表编拟试验等亦可参照使用。

Static measuring methods for test ammunition

GJB 2423A-2009 榴弹发射器定型试验规程

本标准规定了榴弹发射器设计定型试验的要求、试验内容、试验方法与结果评定方法。 本标准适用于各种自动、半自动、非自动榴弹发射器的设计定型试验，其他性质的试验亦可参照使用。

Approval test procedure of grenade launcher

BS ISO 16454:2009 航空航天系统.结构设计.应力分析要求

Space systems - Structural design - Stress analysis requirements

BS ISO 21648:2008 航天系统.飞轮模块设计和试验

Space systems - Flywheel module design and testing

BS ISO 22108:2008 航空系统.飞行器中非飞行项目.识别和控制

Space systems - Non-flight items in flight hardware - Identification and control

BS ISO 22663:2007 航空数据和信息传输系统.接近1的航空链接协议.数据链接层

Space data and information transfer systems - Proximity-1 space link protocol - Data link layer

BS ISO 24638:2008 航空系统.分压力和压力系统集成

Space systems - Pressure components and pressure system integration

ASTM E1548-09 航天污染控制计划的编制的标准实施规程

1.1 This practice is intended to assist in the preparation of formal plans for contamination control, especially of aerospace critical surfaces. Requirements may be established at the systems level, either by the customer or the systems integrator, or at the subsystem level. Subsystem requirements may be imposed by the responsible subsystem supplier or they may be flowed down from the systems organization (4.7). The extent of detail and level of cleanliness required can vary with the particular application and type of hardware being built, but all aspects of contamination control must be included in a final plan. Therefore, each of the following elements must be considered for inclusion in a contamination control plan (CCP): 1.1.1 Cleanliness requirements for deliverable hardware addressing particulate, molecular, or biological contaminants or combination thereof. Specify contamination limits and any budget allocations. 1.1.2 Implementation plans to achieve, verify, and maintain the specified cleanliness requirements. Specify material and process controls, cleaning techniques, verification tests, protection and prevention plans, transportation controls, and corrective action for discrepancies. 1.1.3 Environmental controls including clean facilities to be used, facility maintenance, and monitoring schedule. 1.1.4 Personnel and operational controls including operating procedures, restrictions, training, motivation, and organizational responsibilities including the organization or individual for implementation and verification of the CCP. 1.2 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.

Standard Practice for Preparation of Aerospace Contamination Control Plans

ASTM F2746-09 轻型运动飞机的飞行员操作手册(POH)的标准规范

1.1 This specification provides the minimum requirements for a Pilot’s Operating Handbook (POH) for an aircraft designed, manufactured, and operated as a light sport aircraft. 1.2 This specification defines the POH information that shall be provided by the aircraft manufacturer of a new airplane or airplane kit as a part of the initial sale or transfer to the first- end user. Note 18212;The POH may also be referred to as an Aircraft Operating Instruction (AOI). However, POH is considered the approved nomenclature. 1.3 This specification applies to an airplane seeking civil aviation authority approval, in the form of flight certificates, flight permits, or other like documentation as a light sport aircraft. 1.4 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.

Standard Specification for Pilotx2019;s Operating Handbook (POH) for Light Sport Airplane

ASTM E2695-09 用飞行时间二次离子质谱法说明质谱数据获取的标准指南

Interpretation of static SIMS mass spectral data can be complicated due to the complexity and density of data obtained and therefore, variability often occurs when users are not consistent in their methods of data interpretation This guide is intended to help avoid these inconsistencies, by discussing the most commonly observed scenarios in static SIMS analysis and how to approach these scenarios. This guide can be used as a training guide for employees or students, or both.1.1 This guide provides time-of-flight secondary ion mass spectrometry (ToF-SIMS) users with a method for forms of interpretation of mass spectral data. This guide is applicable to most ToF-SIMS instruments and may or may not be applicable to other forms of secondary icon mass spectrometry (SIMS). 1.2 This guide does not purport to address methods of sample preparation. It is the responsibility of the user to adhere to strict sample preparation procedures in order to minimize contamination and optimize signals. See Guide E1078 and ISO 18116 for sample preparation guidelines. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.4 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.

Standard Guide for Interpretation of Mass Spectral Data Acquired with Time-of-Flight Secondary Ion Mass Spectroscopy

ANSI/IEEE 1559:2009 惯性系统术语标准

The objective is to provide a source of definitions of terminology used in the developemnt, manufacture, and test of aided and unaided inertial systems used for navigation, guidance, orientation, stabilization, and related applications.

Standard for Inertial Systems Terminology

ASTM F319-09 航空航天用透明加热元件中裂纹的偏振光检测标准实施规范

This practice is useful as a screening basis for acceptance or rejection of transparencies during manufacturing so that units with identifiable flaws will not be carried to final inspection for rejection at that time. This practice may also be employed as a go-no go technique for acceptance or rejection of the finished product. This practice is simple, inexpensive, and effective. Flaws identified by this practice, as with other optical methods, are limited to those that produce temperature gradients when electrically powered. Any other type of flaw, such as minor scratches parallel to the direction of electrical flow, are not detectable.1.1 This practice covers a standard procedure for detecting flaws in the conductive coating (heater element) by the observation of polarized light patterns. 1.2 This practice applies to coatings on surfaces of monolithic transparencies as well as to coatings imbedded in laminated structures. 1.3 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard. 1.4 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 precautionary statements see Section 6.

Standard Practice for Polarized Light Detection of Flaws in Aerospace Transparency Heating Elements

ASTM E2373-09 采用超声衍射时差法的标准实施规程

This practice provides general principles for the application of the Time-of-Flight Diffraction Technique as a tool for detection and sizing of discontinuities. TOFD is a nondestructive ultrasonic examination technique that is not based on amplitude response. However, sufficient sensitivity is required to identify indications for evaluation. Techniques used are typically applied to welded joints in carbon steel but the principles may be applicable to other applications including other materials with suitable validation procedures agreeable to the contracting parties. In addition to a stand-alone ultrasonic detection technique TOFD may be used in conjunction with weld examinations such as those described in Practices E 164 and E 1961 where it may be used to improve sizing estimates of flaws detected by the manual or mechanized pulse-echo techniques and help discriminate between flaws and geometric reflectors. The technique has proven effective on thicknesses from 9 to 300 mm (0.375 to 12 in.). TOFD has been used on thicknesses outside of this range but special considerations are necessary. Techniques developed outside of this range of thickness shall be demonstrated as capable of meeting the required detection and sizing requirements of the specification used.1.1 This practice establishes the requirements for developing ultrasonic examination procedures using the ultrasonic technique known as Time-of-Flight Diffraction (TOFD). 1.2 Consistent with ASTM Policy, TOFD may be regarded as an ultrasonic test method whereby the qualities and characteristics of the item tested are evaluated, measured and in some cases identified. Measurements may be subject to precision and bias that may be determined statistically or as a function of some parameter(s) such as wavelength. This practice may be used for applications that would be qualitative and properly addressed as examinations as well as quantitative and more properly addressed as tests. 1.3 The values stated in SI units are to be regarded as standard. Inch-pound units are provided for information. 1.4 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.

Standard Practice for Use of the Ultrasonic Time of Flight Diffraction (TOFD) Technique

ASTM E1559-09 航天器材料污染脱气特性的标准试验方法

1.1 This test method covers a technique for generating data to characterize the kinetics of the release of outgassing products from materials. This technique will determine both the total mass flux evolved by a material when exposed to a vacuum environment and the deposition of this flux on surfaces held at various specified temperatures. 1.2 This test method describes the test apparatus and related operating procedures for evaluating the total mass flux that is evolved from a material being subjected to temperatures that are between 298 and 398 K. Pressures external to the sample effusion cell are less than 7 × 10−3 Pa (5 × 10−5 torr). Deposition rates are measured during material outgassing tests. A test procedure for collecting data and a test method for processing and presenting the collected data are included. 1.3 This test method can be used to produce the data necessary to support mathematical models used for the prediction of molecular contaminant generation, migration, and deposition. 1.4 All types of organic, polymeric, and inorganic materials can be tested. These include polymer potting compounds, foams, elastomers, films, tapes, insulations, shrink tubing, adhesives, coatings, fabrics, tie cords, and lubricants. 1.5 There are two test methods in this standard. Test Method A uses standardized specimen and collector temperatures. Test Method B allows the flexibility of user-specified specimen and collector temperatures, material and test geometry, and user-specified QCMs. 1.6 The values stated in SI units are to be regarded as the standard. The values given in parentheses are for information only. 1.7 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.

Standard Test Method for Contamination Outgassing Characteristics of Spacecraft Materials

MH/T 2001-2008 民用航空器事故征候

本标准规定了民用航空器（以下简称航空器）事故征候的确定依据。 本标准适用于航空器事故征候的确定。

Civil aircraft incident

DIN EN 3635:2008 航空航天系列.焊接边缘.几何构造

The purpose of this standard is to specify the dimensions and tolerances for orbital-welding fittings, intended for stainless steel fluid pipes to EN 3717.

Aerospace series - Weld lip - Geometrical configuration; German and English version EN 3635:2008

DIN EN 3717:2008 航空航天系列.管.发动机防冻液系统的选择

The present standard gives a selection of external diameters and thicknesses of tubes according to ISO 2964. These tubes shall be used for conveying fluids such as kerosene, oil, air, etc. for engine application.

Aerospace series - Tubes - Selection for engines fluid systems; German and English version EN 3717:2008