V04 基础标准与通用方法 标准查询与下载

GJB 6458.29-2008 火箭炮试验方法 第29部分：电磁兼容性试验

本部分规定了火箭炮电磁兼容性试验的试验项目、试验条件、试验设备和试验方法。 本部分适用于火箭炮的电磁兼容性试验。

Test method of rocket launcher. Part 29: Electromagnetic compatibility test

GJB 6458.14-2008 火箭炮试验方法 第14部分：射程和密集度试验

本部分规定了火箭炮及各类火箭发射装置射程和密集度试验的试验条件、试验准备和试验方法。 本部分适用于火箭炮及各类火箭发射装置的射程和密集度试验。

Test method of rocket launcher. Part 14: Firing range and density test

GJB 6458.15-2008 火箭炮试验方法 第15部分：射击强度、射击稳定性及射击安全性试验

本部分规定了火箭炮射击强度、射击稳定性及射击安全性试验的试验项目、试验条件、试验设备、试验准备和试验方法。 本部分适用于火箭炮射击强度、射击稳定性及各种不同发射阵地的射击安全性试验。

Test method of rocket launcher. Part 15: Firing intensity, firing stability and firing safety test

QJ 1556B-2008 元器件质量与可靠性信息采集卡填写规定

本标准规定了航天用电气、电子和机电元器件（以下简称元器件）质量与可靠性信息采集卡的格式和填写要求。 本标准适用于元器件保证全过程主要质量与可靠性信息的采集。

Rules for filling in parts quality and reliability information collection card

GJB 6458.17-2008 火箭炮试验方法 第17部分：战斗操作室安全性试验

本部分规定了火箭炮战斗操作室安全性试验的试验条件、试验准备和试验方法。 本部分适用于火箭炮战斗操作室安全性试验。

Test method of rocket launcher. Part 17: Safety function test of combating operation cab

GJB 6458.12-2008 火箭炮试验方法 第12部分：适航性试验

本部分规定了火箭炮适航性试验的试验条件、试验设备和试验方法。 本部分适用于两栖火箭炮适航性试验。

Test method of rocket launcher. Part 12: Navigation adaptability test

SAE ARP5624-2008 飞行器飞行中结冰现象术语

This SAE Aerospace Recommended Practice (ARP) provides recommended definitions for terms commonly used in aircraft inflight icing system design and analysis, research, and operations. Some general thermodynamic terms are included that are frequently used in icing analysis, but this document is not meant to be an inclusive list of such terms.

Aircraft Inflight Icing Terminology

AIA/NAS NAS 410-2008 无损检验人员REV3的NAS认证和资格[被代替:空军MIL-STD-410 E CANC通告2、空军MIL-STD-410 E CANC通告1、空军 MIL-STD-410 E、空军MIL-STD-410 D通告2、空军MIL-STD-410 D通告]

1.1 PURPOSE: This standard establishes the minimum requirements for the qualification and certification of personnel performing nondestructive testing (NDT), nondestructive inspection (NDI), or nondestructive evaluation (NDE) in the aerospace manufacturing, service, maintenance and overhaul industries. For the purposes of this standard, the term NDT will be used and will be considered equivalent to NDI and NDE. In Europe, the term “approval” is used to denote a written statement by an employer that an individual has met specific requirements and has operating approval. Certification per EN ISO/CEI 17024 is not required by this standard unless specified by local or regulatory requirements. The term “certification” as defined in paragraph 3.1 is used throughout this standard as a substitute for the term “approval”. Except when otherwise specified in the written practice, certification in accordance with this standard includes operating approval. 1.2 APPLICABILITY: This standard applies to personnel using NDT methods to test and/or accept materials, products, components, assemblies or sub-assemblies. This standard also applies to personnel directly responsible for the technical adequacy of the NDT methods used, who write NDT procedures and/or work instructions, who audit NDT facilities, or who provide technical NDT support or training. This standard does not apply to individuals who only have administrative or supervisory authority over NDT personnel or to research personnel developing NDT technology for subsequent implementation and approval by a certified Level 3. Personnel performing specialized inspections using certain direct readout instruments as determined by a Level 3 certified in the method, do not require qualification or certification to this standard. 1.2.1 IMPLEMENTATION: This standard addresses the use of a National Aerospace NDT Board (NANDTB). NANTDBs are only used as specified herein and it is not mandatory to have such a board for compliance with this document. Personnel certified to previous revisions of NAS 410 or EN 4179 need not recertify to the requirements of this standard until their current certification expires. 1.3 COMMON METHODS: This standard contains detailed requirements for the following common NDT methods: Liquid penetrant (PT) Magnetic particle (MT) Eddy current (ET) Ultrasonic (UT) Radiography (RT) Thermography (IRT) Shearography (ST) 1.3.1 OTHER METHODS: When invoked by engineering, quality, cognizant engineering organization or prime contractor requirements, this standard applies to other current and emerging NDT methods used to determine the acceptability or suitability for intended service of a material, part, component, sub-assembly or assembly. Such methods may include, but are not limited to, acoustic emission, neutron radiography, leak testing and holography. The requirements for personnel training, experience, and examination for these other methods shall be established in accordance with paragraph 6.4 and shall be documented by the employer.

NAS Certification& Qualification of Nondestructive Test Personnel REV 3 [Replaced: AIR FORCE MIL-STD-410 E CANC NOTICE 2, AIR FORCE MIL-STD-410 E CANC NOTICE 1, AIR FORCE MIL-STD-410 E, AIR FORCE MIL-STD-410 D NOTICE 2, AIR FORCE MIL-STD-410 D NOTIC

SAE AIR5656-2008 统计学稳定性评估

This SAE Aerospace Information Report (AIR) provides a methodology for performing a statistical assessment of gasturbine- engine stability-margin usage. Consideration is given to vehicle usage, fleet size, and environment to provide insight into the probability of encountering an in-service engine stall event. Current industry practices, such as ARP1420, supplemented by AIR1419, and engine thermodynamic models, are used to determine and quantify the contribution of individual stability threats. The statistical technique adopted by the S-16 committee for performing a statistical stability assessment is the Monte Carlo method (see Applicable References 1 and 2). While other techniques may be suitable, their application is beyond the scope of this document. The intent of the document is to present a methodology and process to construct a statistical-stability-assessment model for use on a specific system and its mission or application. The purpose of the Statistical Stability Assessment (SSA) is to provide a quantitative tool for optimizing engine stability margin requirements and provide greater visibility of off-design conditions. It can be applied at the inception of a new project to perform trade studies and support risk assessments; or to a mature project to assess the impact/risk of modifications or changes in operational usage. This document provides guidelines on the procedures and data that are required to perform the statistical stability assessment. A number of illustrative examples are presented.

Statistical Stability Assessment

SAE AIR5866-2008 平面波的评估

"An Assessment of Planar Waves" provides background on some of the history of planar waves, which are timedependent variations of inlet recovery, as well as establishing a hierarchy for categorizing various types of planar waves. It further identifies approaches for establishing compression-component and engine sensitivities to planar waves, and methods for accounting for the destabilizing effects of planar waves. This document contains an extensive list and categorization (see Appendix A) of references to aid both the newcomer and the practitioner on this subject. The committee acknowledges that this document addresses only the impact of planar waves on compression-component stability and does not address the impact of planar waves on augmenter rumble, engine structural issues, and/or pilot discomfort.

An Assessment of Planar Waves

ASTM F312-08 膜滤器上航空流体中颗粒微观大小的测定及计数的标准试验方法

Reported particle size measurement is a function of both the actual particle dimension and shape factor as well as the particular physical or chemical properties of the particle being measured. Caution is required when comparing data from instruments operating on different physical or chemical parameters or with different particle size measurement ranges. Sample acquisition, handling and preparation can also affect the reported particle size results.1.1 These test methods cover the determination of the size distribution and quantity of particulate matter contamination from aerospace fluids isolated on a membrane filter. The microscopical techniques described may also be applied to other properly prepared samples of small particles. Two test methods are described for sizing particles as follows: 1.1.1 Test Method A8212;Particle sizes are measured as the diameter of a circle whose area is equal to the projected area of the particle. 1.1.2 Test Method B8212;Particle sizes are measured by their longest dimension. 1.2 The test methods are intended for application to particle contamination determination of aerospace fluids, gases, surfaces, and environments. 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 These test methods do not provide for sizing particles smaller than 5 μm. Note 18212;Results of these methods are subject to variables inherent in any statistical method. The use of these methods as a standard for initially establishing limits should be avoided unless ample tolerances are permissible. 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 health practices and determine the applicability of regulatory limitations prior to use.

Standard Test Methods for Microscopical Sizing and Counting Particles from Aerospace Fluids on Membrane Filters

ASTM E1235-08 宇宙飞船在环境受控范围内的非挥发残留物 (NVR) 重量分析测定的标准试验方法

The NVR determined by this test method is that amount that can reasonably be expected to exist on hardware exposed in environmentally controlled areas. The evaporation of the solvent at or near room temperature is to quantify the NVR that exists at room temperature. Numerous other methods are being used to determine NVR. This test method is not intended to replace methods used for other applications.1.1 This test method covers the determination of nonvolatile residue (NVR) fallout in environmentally controlled areas used for the assembly, testing, and processing of spacecraft. 1.2 The NVR of interest is that which is deposited on sampling plate surfaces at room temperature: it is left to the user to infer the relationship between the NVR found on the sampling plate surface and that found on any other surfaces. 1.3 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. 1.4 The values stated in SI units are to be regarded as standard. No other units of measurement are included in this standard.

Standard Test Method for Gravimetric Determination of Nonvolatile Residue (NVR) in Environmentally Controlled Areas for Spacecraft

ASTM F311-08 用膜滤器进行粒状污染物分析用航空航天流体样品的处理

This practice provides for the processing of liquid samples obtained in accordance with Practice F 302 and Practices F 303. It will provide the optimum sample processing for visual contamination methods such as Method F 312, and Test Method F 314.1.1 This practice covers the processing of liquids in preparation for particulate contamination analysis using membrane filters and is limited only by the liquid-to-membrane filter compatibility. 1.2 The practice covers the procedure for filtering a measured volume of liquid through a membrane filter. When this practice is used, the particulate matter will be randomly distributed on the filter surface for subsequent contamination analysis methods. 1.3 The practice describes procedures to allow handling particles in the size range between 2 and 1000 μm with minimum losses during handling. 1.4 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 Processing Aerospace Liquid Samples for Particulate Contamination Analysis Using Membrane Filters

BS ISO 21349:2007 航空航天系统.规划评定

ISO 21349:2007 provides process requirements for project reviews as a set of required functions. The requirements and recommendations cover the function inputs, outputs, mechanisms, and controlling conditions. It is intended for use in implementing the review requirements of ISO 14300-1, ISO 14300-2, ISO 15865, and such other space systems and operations standards that require formal reviews. ISO 21349:2007 specifies the responsibilities of a review board and gives guidance concerning review board composition. ISO 21349:2007 is applicable to reviews for a project at any level within a larger project, as well as for major milestone reviews at the top level of a major project. It is intended to be used either by an independent developer as a basis for enterprise processes, or as a basis for an agreement between a supplier and a customer. ISO 21349:2007 also provides normative descriptions of the kinds of reviews that are commonly useful in assuring the success of a space project.

Space systems. Project reviews

BS ISO 19933:2007 航空航天系统.航天器发射环境试验报告用格式

ISO 19933:2007 provides a specific format to report the test process and results of spacecraft (SC) qualification to the launch environment. The following types of tests are considered: static load; modal survey; sine vibration; acoustic noise; random vibration; shock; and electromagnetic compatibility (EMC). The definition of test specifications and test requirements are derived from launch vehicle (LV) user's manuals as defined in ISO 14303. Only those tests that are intended to demonstrate the compliance of a given SC design with its LV environment are taken into consideration.

Space systems. Format for spacecraft launch environment test report

ISO 22010:2007 航空航天系统.质量特性控制

This International Standard describes a process for managing, controlling and monitoring the mass properties of space systems. The relationship between this management plan and the performance parameters for mass properties to be met throughout the mission is described. Ground handling, dynamics analysis and test setups that rely on accurate mass properties inputs are identified. This International Standard covers all programme phases from pre-proposal through to end of life.

Space systems - Mass properties control

KS W 0638-2007 空气动力学.概念、量和符号.第3部分:力、力矩及其系数和导数

이 규격은 힘 및 모멘트의 도함수 및 그들의 힘 및 모멘트의 특성을 표시하는 기타 양의 도

Flight dynamics-Concepts, quantities and symbols-Part 3:Derivatives of forces, moments and their coefficients

ISO 16454:2007 航天系统.结构设计.应力分析要求

This International Standard is intended to be used for the determination of the stress/strain distribution and margins of safety in launch vehicles and spacecraft primary structure design. Liquid propellant engine structures, solid propellant engine nozzles and the solid propellant itself are not covered, but liquid propellant tanks, pressure vessels and solid propellant cases are within the scope of this International Standard. This International Standard provides requirements for the determination of maximum stress and corresponding margin of safety under loading, and defines criteria for static strength failure modes, such as rupture, collapse and detrimental yielding. Critical conditions associated with fatigue, creep and crack growths are not covered. Notwithstanding these limitations in scope, the results of stress calculations based on the requirements of this International Standard are applicable to other critical condition analyses. In accordance with the requirements of this International Standard, models, methods and procedures for stress determination can also be applied to the displacements and deformation calculations, as well as to the loads definition, applied to substructures and structural members of structures under consideration. When this International Standard is applied, it is assumed that temperature distribution has been determined and is used as input data.

Space systems - Structural design - Stress analysis requirements

REG CAP 455-2007 耐飞性通告

Airworthiness Notices are issued by the Civil Aviation Authority to circulate information to all concerned with the airworthiness of civil aircraft. Mandatory Airworthiness Notices that were previously published in CAP 455 have been transferred to CAP 747 – Mandatory Requirements for Airworthiness and are now published as Generic Requirements in Appendix 1. This document can be located via the CAA website at www.caa.co.uk/publications

Airworthiness Notices

KS W ISO 2685:2007 航空器.机载设备的环境试验程序.指定防火区的防火

이 규격은 “화재 구역(fire zone)”이라고 지정된 구역에 있는 항공기의 모든 구성품

Aircraft－Environmental test procedure for airborne equipment－Resistance to fire in designated fire zones