V00 标准化、质量管理 标准查询与下载

GB/T 43370-2023 民用无人机地理围栏数据技术规范

Technical Specifications for Geofencing Data for Civilian UAVs

GB/T 29076-2021 航天产品质量问题归零实施要求

本文件规定了航天产品质量问题归零的一般要求、程序、技术归零工作要求和管理归零工作要求等内容。 本文件适用于航天产品设计、生产、试验、使用等各阶段中发生的质量问题归零工作。

Execution requirements of quality problem closed loop for aerospace product

GB/T 38931-2020 民用轻小型无人机系统安全性通用要求

规范性引用文件pe 术语和定义一般要求4.1 工作目标4.2 ”基本原则4.3 工作过程详细要求5.1 安全性要求分解5.2 初步危险分析5.3 ”安全性设计准则制定5.4 系统危险分析5.5 试验的安全5.6，使用与保障危险分析必co

General requirements for safety of civil small and light unmanned aircraft system

GB/T 38905-2020 民用无人机系统型号命名

本标准规定了民用无人机系统型号的命名组成和命名方法。本标准适用于民用无人机系统行业管理.研制生产.销售、使用维护的型号命名。

Type designation for civil unmanned aircraft system

GB/T 32299-2015 航天项目风险管理

Space project risk management

GB/T 29076-2012 航天产品质量问题归零实施要求

本标准规定了航天产品质量问题归零的实施要求。 质量问题归零包括了质量问题技术归零和质量问题管理归零。 本标准适用于航天产品从初样阶段开始各阶段的质量问题技术归零和管理归零。

Execution requirements for quality problem close loop of aerospace product

GB/T 29072-2012 航天器研制技术流程编写规则

本标准规定了航天器研制技术流程(以下简称技术流程)的相关术语、编写原则、编写依据、技术流程分类、编写要求和内容、编写步骤和编写方法、本标准适用于航天器系统、分系统工作项目技术流程的编写、设备研制技术流程的编写可参照使用、

Drafting rules of technical network for spacecraft development

GB/T 29073-2012 航天器研制计划流程编写规则

本标准规定了航天器研制計劃流程的相關術語、編寫原則、編寫依據、計劃流 程體系 內容及編寫步骤等要求。 本标准适用于按层次划分的航天器系统级、分系统级.设备级和工作项目(含软件?计划流程的编 写，也适用于按时间划分的航天器研制全过程、阶段和年度等计划流程的编写。

Drafting rules of schedule network for spacecraft development

GB/T 29076-2012e 航天产品质量问题归零实施要求

Execution requirements for quality problem close loop of aerospace product

GB/T 29073-2012(英文版) 航天器研制进度网络规则起草

Drafting rules of schedule network for spacecraft development

GB/T 29072-2012(英文版) 航天器研制技术网络规则起草

Drafting rules of technical network for spacecraft development

DB43/T 2779-2023 无人机应用服务通用规范

General specifications for UAV application services

DIN 5452-1:2021 航空航天系列. 无人机系统（UAS）. 第1-0部分: 术语和定义; 德文和英文文本

This document specifies terms and definitions in the field of unmanned aircraft systems that are used by private, commercial users and by those under public law as well as manufacturers. In addition to that regulating and supervisory authorities as well as testing institutes are

Aerospace series - Unmanned aircraft systems (UAS) - Part 1: Terms and definitions; Text in German and English

DIN EN 16602-60-14:2020 航天产品保证. 重新安装程序. EEE 组件; 英文版 EN 16602-60-14-2020

This standard specifies the requirements, also known as \

Space product assurance - Relifing procedure - EEE components; English version EN 16602-60-14:2020

HB 8569-2020 民用飞机构型管理要求

Configuration management requirements for civil aircraft

ASTM F3174/F3174M-19 确定飞机操作限制和信息的标准规范

1.1 This specification covers airworthiness requirements for establishing general limitations and information to be contained in the aeroplane flight manual. This specification specifies what information shall be provided and does not state how such information shall be presented unless this is necessary for the clarity of the purpose of the specification. Refer to Specification F3117/F3117M for means and methods of presentation. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Level 1, 2, 3, and 4 Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this specification are: Limitations for Airspeed, Weight and Center of Gravity, Auxiliary Power Units, Minimum Flight Crew, Maximum Passenger Seating Configuration, Kinds of Operation, and Maximum Operating Altitude. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this specification (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 web page (www.astm.org/COMMITTEE/F44.htm). 1.3 Units—This specification may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance with the 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 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 Establishing Operating Limitations and Information for Aeroplanes

ASTM F3245-19 飞机电子技术人员认证的标准指南

4.1 The guide is intended to be used to assess competencies of qualified individuals who wish to become certified as an Aircraft Electronics Technician through a certification program. 4.2 The guide is intended to be used in concert with a certification provider’s structure and materials for management, exam delivery, and candidate preparation. 1.1 The purpose of this guide is to address the basic fundamental subject knowledge, task performance, and task knowledge activities and functions for avionics professionals to be titled Aircraft Electronics Technicians (AETs). 1.2 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. 1.3 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 Guide for Aircraft Electronics Technician Personnel Certification

ASTM F3180/F3180M-19 飞机低速飞行特性标准规范

1.1 This specification covers the low-speed flight characteristics of fixed-wing aircraft and provides standards for departure characteristics, spinning, and stall warning. The material was developed through open consensus of international experts in general aviation. This information was created by focusing on Normal Category aeroplanes. The content may be more broadly applicable; it is the responsibility of the Applicant to substantiate broader applicability as a specific means of compliance. The topics covered within this specification are: (4.1) Low-Speed Flight Characteristics Score, (4.2) Stall Characteristics, (4.3) Stall Warning, (4.4) Departure Characteristics: Single Engine, (4.5) Departure Characteristics: Multiengine, (4.6) Spinning, and (4.7) Safety-Enhancing Features. 1.2 An applicant intending to propose this information as Means of Compliance for a design approval must seek guidance from their respective oversight authority (for example, published guidance from applicable CAAs) concerning the acceptable use and application thereof. For information on which oversight authorities have accepted this standard (in whole or in part) as an acceptable Means of Compliance to their regulatory requirements (hereinafter “the Rules”), refer to the ASTM Committee F44 webpage (www.astm.org/COMMITTEE/F44.htm). 1.3 Units—This standard may present information in either SI units, English Engineering units, or both; the values stated in each system may not be exact equivalents. Each system shall be used independently of the other; combining values from the two systems may result in nonconformance with the 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, health, and environmental practices and determine the applicability of regulatory limitations prior to use. 1.5 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 Low-Speed Flight Characteristics of Aircraft

DB61/T 1223-2018 制造成熟度评价程序

本标准适用于制造成熟度评价工作

Manufacturing Maturity Assessment Program

DB61/T 1222-2018 制造成熟度等级及评价准则

本标准适用于产品、组件或零部件制造成熟度的评价

Manufacturing Maturity Levels and Evaluation Criteria