基础标准与通用方法标准-分析测试百科网

BS ISO 19923:2017 航天环境(天然和人造). 生成航天器最坏情况下电势差的等离子体环境

Space environment (natural and artificial). Plasma environments for generation of worst case electrical potential differences for spacecraft

ICS: 49.140
CCS: V04
发布: 2017-06-28
实施: 2017-06-28

BS ISO 16192:2017 空间系统在太空项目中获得的经验（吸取的教训）原则和指南

Space systems. Experience gained in space projects (lessons learned). Principles and guidelines

ICS: 49.020;49.140
CCS: V04
发布: 2017-05-05
实施: 2017-05-05

DIN EN 16602-10:2017 航空航天系列.航天产品保证.产品保证管理;英文版本EN 16602-10-2017

Space product assurance - Product assurance management; English version EN 16602-10:2017

ICS: 49.140
CCS: V04
发布: 2017-05
实施

ISO 16192:2017 航天系统.空间计划中的经验获取(经验学习).原则和指南

This document outlines lessons learned principles and guidelines that are applicable in all space project activities (management, technical, quality, cost and schedule). The application of this document is intended to be included in the supplier quality management system, but can be tailored in individual contracts as agreed by the customer and supplier, depending on: — the content of each project (size, technological level and novelty, particular organization, participants, etc.); — the interest and usefulness of the related information. The lessons learned information can result from any situation which might be encountered in similar contexts for future projects, i.e.: — undesirable experiences that need to be avoided; — strategies, rules, principles of design, validation, tests and operations that proved to be successful or necessary. This document neither endorses nor recommends the transmission of company proprietary information to external entities as part of a lessons learned process. Implementing a formal lessons learned process as outlined in this document makes it possible to capture and benefit from this information. The lessons learned activity is an important contribution to the processing of the preventive and corrective actions specified in ISO 9001 and ISO 17666. This document also provides lessons learned processes and suggested lessons learned forms.

Space systems - Experience gained in space projects (lessons learned) - Principles and guidelines

ICS: 49.020;49.140
CCS: V04
发布: 2017-04
实施

ISO 15872:2017 航空航天.UNJ螺纹.测量

This document provides methods for the gauging of ISO UNJ threads complying with ISO 3161. Other methods of ensuring that the product is within the specified limits can be used, provided that correlation with the specified gauges is established.

Aerospace - UNJ threads - Gauging

ICS: 49.030.10
CCS: V04
发布: 2017-03
实施

BS EN 16602-10:2017 航空产品保证.产品保证管理

Space product assurance. Product assurance management

ICS: 49.140
CCS: V04
发布: 2017-02-28
实施: 2017-02-28

ISO 19826:2017 航空航天系统. 项目管理. 产品特征管理

Space systems - Programme management - Management of product characteristics

ICS: 49.140
CCS: V04
发布: 2017-02-01
实施

BS EN 4179:2017 航空航天系列.无损检验人员的资格和审批

Aerospace series. Qualification and approval of personnel for non-destructive testing

ICS: 49.020
CCS: V04
发布: 2017-01-31
实施: 2017-01-31

ASTM F3082/F3082M-17 飞机重量和重心的标准规格

1.1 This specification establishes the airworthiness design standards associated with aeroplane weight and center of gravity. 1.2 The term “aeroplane” is utilized in this specification as it was originally conceived for normal category fixed wing aircraft with a maximum certificated weight of 19 000 lb or less and a passenger seating configuration up to 19 as defined in the Rules. However, these standards may be more broadly applicable and their usage should not be unnecessarily limited. 1.3 The applicant for a design approval shall seek the individual guidance of their respective civil aviation authority (CAA) body concerning the use of this specification as part of a certification plan. For information on which CAA regulatory bodies have accepted this specification (in whole or in part) as a means of compliance to their small aircraft airworthiness regulations (hereinafter referred to as “the Rules”), refer to ASTM Committee F44 webpage (www.astm.org/COMMITTEE/F44.htm), which includes CAA website links. 1.4 Units—The values stated in either SI units or inch-pound units are to be regarded separately as standard. The values stated in each system may not be exact equivalents; therefore, each system shall be used independently of the other. Combining values from the two systems may result in non-conformance with the standard. 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.6 This international standard was developed in accordance with internationally recognized principles on standardization established in the Decision on Principles for the Development of International Standards, Guides and Recommendations issued by the World Trade Organization Technical Barriers to Trade (TBT) Committee.

Standard Specification for Weights and Centers of Gravity of Aircraft