V07 电子计算机应用 标准查询与下载

QJ 20031-2011 航天办公系统电子公文交换格式

本标准规定了航天内部各单位网络办公系统间电子公文交换过程中的数据组成，并对数据每层元素的XML标记、定义、值域和Schema定义等加以描述。 本标准适用于航天内部各单位网络办公系统间电子公文的交换。其它军工集团电子公文交换、传输也可参照使用。

Specification for the structure of exchange of electronic official document between office automatic system in aerospace enterprises

QJ 20055-2011 航天产品数据管理（PDM）实施指南

本标准规定了航天企业实施航天产品数据管理系统的需求分析、队伍组织、实施阶段、实施工作等内容。 本标准适用于开发和实施AVIDM系统的企业。使用其它PDM系统的航天企业可参照执行。

Implementation guide for aerospace product data management(PDM)

QJ 20056-2011 航天档案数据元

本标准规定了航天档案业务管理中主要数据元及其描述。 本标准适用于航天档案信息管理系统的建设与维护，以及档案信息的表达与交换。

Data elements of aerospace archives

QJ 20063-2011 异构数据库数据接口要求

本标准规定了异构数据库数据访问的语句结构和数据结构、异构数据库透明访问的格式规范、对异构数据库进行数据交换的数据结构等异构数据库数据接口方面的要求。 本标准适用于异构数据库接口开发以及应用中对异构数据库数据进行一致性的透明访问。

Requirements of data interface for heterogenous database

ISO 14300-1:2011 航天系统.项目管理.第1部分:项目建设

Space systems - Programme management - Part 1: Structuring of a project

ISO 27852:2011 航天系统.轨道寿命预估

Space systems - Estimation of orbit lifetime

ISO 17566:2011 空间系统.一般测试文档

Space systems - General test documentation

SAE AS5725A-2011 微型航天飞行存储接口标准

This standard defines implementation requirements for the electrical interface between: a. aircraft carried miniature store carriage systems and miniature stores; b. aircraft parent carriage and miniature stores; c. surface based launch systems and miniature stores The interface provides a common interfacing capability for the initialization and employment of smart miniature munitions and other miniature stores from the host systems. Physical, electrical, and logical (functional) aspects of the interface are addressed. The purpose of this standard is to minimize proliferation of electrical interfaces between platforms, miniature stores and associated carriage systems and thereby promote interoperability of miniature stores and carriage systems across different programs and services. This standard applies to all platforms, miniature stores and associated carriage systems that electrically interface with each other. The carriage systems include captive and releasable (canister type) aircraft mounted carriage devices, platforms such as unmanned combat air vehicles (parent carriage), dedicated carriage areas on aircraft, and surface based launch systems. For simplicity within this document, all carrying devices are generically referred to as the miniature store carriage system (or simply carriage system) from an interface perspective. Additionally, the term store as used in this document refers to a miniature store unless otherwise indicated.

Interface Standard, Miniature Mission Store Interface

DIN EN 9300-003:2011 航空航天系列. LOTAR. 数字技术产品文档 (如3D, CAD及PDM数据) 的长期存档和检索. 第003部分:基础和概念; 德文和英文版本EN 9300-003-2010

Aerospace series - LOTAR - Long term archiving and retrieval of digital technical product documentation such as 3D, CAD and PDM data - Part 003: Fundamentals and concepts; German and English version FprEN 9300-003:2010

ISO 11893:2011 航空航天系统.程序管理.项目组织

This International Standard defines the project organization principles and requirements needed to provide satisfactory and coherent management of space projects. The general requirements for project organization are given in ISO 14300-1. This International Standard addresses the following, in particular: a) responsibility and authority of the actors (all actors, customer, supplier), b) interrelations between the actors (meetings, action monitoring, reporting, assessments and audits), c) information technologies, and d) project organization documentation. The requirements specified herein apply to and affect the supplier and customer at all levels. This International Standard is applicable to the customer-supplier relationship for space products to the extent agreed by both parties. It is intended to be used as a basis when establishing and negotiating customer program/project management requirements and to guide the supplier's responses. When viewed in a specific project context, the requirements defined in this International Standard should be tailored to match the specific requirements of a particular profile and circumstances of a project.

Space systems - Programme management - Project organization

BS ISO 27026:2011 航空航天系统.程序管理.项目管理架构的故障

Space systems. Programme management. Breakdown of project management structures

ISO 23460:2011 航空航天项目.程序管理.可靠保证要求

This International Standard presents the requirements for a dependability (reliability, availability and maintainability) assurance programme for space projects. It defines the dependability requirements for space products as well as for system functions implemented in software, and the interaction between hardware and software. The provisions of this International Standard apply to all programme phases.

Space projects - Programme management - Dependability assurance requirements

ISO 27026:2011 空间系统.规划管理.项目管理结构故障

This International Standard specifies processes, requirements and recommendations for the breakdown of project management structures, collectively called project breakdown structures, in terms of the various specification (i.e. requirements), functional, product, work, cost, business and organizational breakdown structures that are established and implemented to contribute to the success of a space programme, which is often composed of one or more projects. It is intended to complement and supplement similar project breakdown structure processes, requirements and recommendations contained within ISO 14300-1, which serves as a higher tier International Standard for this International Standard and for such other space systems and operations International Standards that require formal project breakdown structures. This International Standard specifies the various types of project breakdown structures and gives processes, requirements and guidance concerning the composition of these breakdown structures. This International Standard is applicable to project breakdown structures for a project, including at the top level of a programme, i.e. level 0, as indicated in ISO 14300-1. It is intended to be used either by an independent developer as a partial basis for programme processes or as a basis for an agreement between a supplier and a customer. This International Standard also provides descriptions of the kinds of project breakdown structures that are commonly useful in contributing to the success of a space project. Other project breakdown structures not described in this International Standard also often contribute to the success of a space project.

Space systems - Programme management - Breakdown of project management structures

SAE AS6003-2011 TTP通信协议

This SAE Aerospace Standards (AS) establishes the specification for TTP communication protocol functionality as a core networking component for design of synchronous, time-triggered distributed real-time communication networks. This document is referred to as the "base" specification, containing the generic specification of TTP communication protocol functionality, and frame formats, communication services and protocol state machines with transitions, TTP node operation, TTP network operation, distributed clock synchronization and error detection on the network layer. The details described in this standard enable interoperable TTP controller implementations.

TTP Communication Protocol

ANSI/AIAA S-131-2011 天体动力学.传播规范,测试案例和推荐的操作规程

This document provides the broad astrodynamics and space operations community with technical standards and lays out recommended approaches to ensure compatibility between organizations. Applicable existing standards and accepted documents are leveraged to make a complete - yet coherent - document. These standards are intended to be used as guidance and recommended practices for astrodynamics applications in Earth orbit where interoperability and consistency of results is a priority. For those users who are purely engaged in research activities, these standards can provide an accepted baseline for innovation.

Astrodynamics - Propagation Specifications, Test Cases, and Recommended Practices

SAE ARP4754A-2010 民航班机和系统研发导则

This document discusses the development of aircraft systems taking into account the overall aircraft operating environment and functions. This includes validation of requirements and verification of the design implementation for certification and product assurance. It provides practices for showing compliance with the regulations and serves to assist a company in developing and meeting its own internal standards by considering the guidelines herein. The guidelines in this document were developed in the context of Title 14 Code of Federal Regulations (14CFR) Part 25 and European Aviation Safety Agency (EASA) Certification Specification (CS) CS-25. It may be applicable to other regulations, such as Parts 23, 27, 29, 33, and 35 (CS-23, CS-27, CS-29, CS-E, CS-P). This document addresses the development cycle for aircraft and systems that implement aircraft functions. It does not include specific coverage of detailed software or electronic hardware development, safety assessment processes, inservice safety activities, aircraft structural development nor does it address the development of the Master Minimum Equipment List (MMEL) or Configuration Deviation List (CDL). More detailed coverage of the software aspects of development are found in RTCA document DO-178B, "Software Considerations in Airborne Systems and Equipment Certification" and its EUROCAE counterpart, ED-12B. Coverage of electronic hardware aspects of development are found in RTCA document DO-254/EUROCAE ED-80, "Design Assurance Guidance for Airborne Electronic Hardware". Design guidance and certification considerations for integrated modular avionics are found in appropriate RTCA/EUROCAE document DO-297/ED-124. Methodologies for safety assessment processes are outlined in SAE document ARP4761, "Guidelines and Methods for Conducting the Safety Assessment Process on Civil Airborne Systems and Equipmen". Details for in-service safety assessment are found in ARP5150, "Safety Assessment of Transport Airplanes In Commercial Service" and ARP5151 Safety Assessment of General Aviation Airplanes and Rotorcraft In Commercial Service. Post-certification activities (modification to a certificated product) are covered in section 6 of this document. The regulations and processes used to develop and approve the MMEL vary throughout the world. Guidance for the development of the MMEL should be sought from the local airworthiness authority.

Guidelines for Development of Civil Aircraft and Systems

DIN CEN/TS 16071:2010 单一欧洲空中下应用的飞行数据处理的互操作性(空中交通管制-空中交通管制).互操作性规则EC 552/2004.德文和英文版本CEN/TS 16071-2010

Interoperability of Flight Data Processing (Air Traffic Control - Air Traffic Control) for application under the Single European Sky - Interoperability Regulation EC 552/2004; German and English version CEN/TS 16071:2010

BS ISO 13537:2010 空间数据和信息传递系统.空间数据系统用基准结构

Space data and information transfer systems. Reference architecture for space data systems

BS ISO 22647:2010 航天数据和信息传输系统.空间链路识别符

Space data and information transfer systems. Space link identifiers

BS ISO 10537:2010 航天数据和信息传送系统.封装业务

Space data and information transfer systems. Encapsulation service