V70 航天器综合 标准查询与下载

GJB 5410-2005 战略导弹末制导系统测试发射规程

本标准规定了战略导弹末制导系统（以下简称“末制导系统”）在发射场执行测试发射任务时的基本要求和测试发射流程。 本标准适用于末制导系统在发射场进行的测试发射飞行试验。合练、抽检、战训等亦可参照执行。

Test and launching rules for terminal guidance system of strategic missile

ISO 21347:2005 航天系统.断裂和损坏控制

This International Standard establishes general requirements for the application of fracture control technology to fracture-critical items (FCIs) fabricated from metallic, non-metallic or composite materials. It also establishes mechanical damage control requirements for mechanical-damage-critical items (MDCIs) fabricated from composite materials. These requirements, when implemented on a particular space system, can assure a high level of confidence in achieving safe operation and mission success. The requirements set forth in this International Standard are the minimum fracture control and mechanical damage control requirements for FCIs and MDCIs in general space systems, including launch vehicles and spacecraft. With necessary modifications, these requirements may also be applicable to reusable launch vehicles (RLVs). This International Standard is not applicable to the Shuttle and its payloads or the ISS and its equipment, since they already have a set of specific requirements suitable for their special applications. This International Standard is not applicable to processing detected defects.

Space systems - Fracture and damage control

ISO 21351:2005 航天系统.功能和技术规范

This document provides an overview of the respective purposes and positions of functional and technical specifications, their required contents, and the process for developing these documents. This document is applicable to all types of space systems, all product elements, and projects.

Space systems - Functional and technical specifications

ARINC 664P8-2005 航行器数据网络部分8协议和服务互用性

AIRCRAFT DATA NETWORK PART 8 INTEROPERATION WITH NON-IP PROTOCOLS AND SERVICES

AIRCRAFT DATA NETWORK PART 8 INTEROPERATION WITH NON-IP PROTOCOLS AND SERVICES

BS EN 14607-1:2005 航天工程.机械.热控制

Space engineering - Mechanical - Thermal control

BS EN 14607-1:2004 航天工程.机械.热控制

EN 14607 Part 1 of Space engineering - Mechanical specifies requirements for the discipline of thermal engineering. This document specifies the requirements for the definition, analysis, design, manufacture, verification and in-service operation of thermal control subsystems of spacecraft and other space products. This document applies to the thermal engineering activities of all spacecraft and space related products for all thermal aspects and temperature levels for space products. For this document, the complete temperature scale is divided into three ranges defined as follows: · Cryogenic temperature range, below 120 K; · Conventional temperature range, between 120 K and 420 K; · High temperature range, above 420 K. The core part of this document concerns the conventional temperature range; complementary information, requirements and definitions for the cryogenic and high temperature range respectively are provided in annexes B and C. When viewed from the perspective of a specific project context, the requirements defined in this document should be tailored to match the genuine requirements of a particular profile and circumstances of a project. NOTE Tailoring is a process by which individual requirements of specifications, standards and related documents are evaluated, and made applicable to a specific project by selection, and in some exceptional cases, modification of existing or addition of new requirements. This document is applicable to: · thermal engineering activities of all space and space related products, covering all thermal engineering aspects involved in the achievement of the required thermal performance, particularly: design, verification, manufacturing and in service operations; · thermal control subsystem and to relevant parts of all space products.

Space engineering Mechanical-Part 1:Thermal control

ARINC 664P5-2005 航行器数据网络部分5网络特性和互相联络

The purpose of ARINC Specification 664: Aircraft Data Network, Part 5 – Network Domain Characteristics and Interconnection, is to provide design and implementation guidelines for networks installed in aircraft. Such networks may be used to allow networ

AIRCRAFT DATA NETWORK PART 5 NETWORK DOMAIN CHARACTERISTICS AND INTERCONNECTION

GJB 2204A-2005 卫星总装通用规范

本规范规定了卫星总装(含功能组件和舱段总装)的原则、要求及质量保证规定。 本规范适用于卫星总装的设计、工艺、实施、质量控制和验收。各种卫星试验模型的总装可参照使用。

General specification for satellite integration

QJ 3221-2005 空间碎片减缓要求

本标准规定了运载器和航天器减少空间碎片的产生、减低空间系统危害程度的要求和应采取的减缓措施。 本标准适用于进入地球轨道的航天器和运载器的设计、发射、运行及任务后处置。

Requirements for space debris mitigation

QJ 3205-2005 地（舰）空导弹武器系统飞行试验大纲编写指南

本标准规定了地（舰）空导弹武器系统飞行试验大纲的基本内容和编写要求。 本标准适用于地（舰）空导弹武器系统研制性飞行试验大纲的编制，定型和批油检飞行试验大纲的编制可参照执行。

Guidelines for drafting flight-test outlines of surface-to-air missile weapon system

SJ 20920-2005 外弹道测量差分多普勒法电离层折射修正系统通用规范

本规范规定了外弹道测量差分多普勒法电离层折射修正系统（以下简称“系统”）的要求、质量保证规定、交货准备等内容。 本规范适用于外弹道测量差分多普勒法电离层折射修正系统的研制、检验与验收。

General specification for the ionospheric refraction correction system for exterior ballistic measurement by differential Doppler

KS W 0629-2004 定货人优先选择的标准及规格

이 규격은 상용 관행과 비정부 규격의 사용에 관한 예산 관리국(OMB) 공보 A-119

Order of preference for the selectionof standard and specification

KS W 0627-2004 航空航天器备品可互换性和可代替性

이 규격은 다음에 열거된 것과 같은 항공 우주선(6.1 참조)에 사용되는 각종 부품,

Interchangeability and replaceability of component partsfor aerospace vehicles

KS W 0632-2004 航空航天器热处理设备和测定高温设备的管理及试验通则

이 규격은 주로 항공 우주용 반제 및 완성 금속 부품의 열 처리에 사용하는 노, 염욕조

Control and test requirements for thermal treatment andpyrometric equipments for aerospace use

KS W 0628-2004 航空器和导弹的电路系统实体模型试验基本要求

이 규격은 항공기 또는 유도탄의 시제기 비행 시험 이전에 수행되는 전기 계통 모크업 시

General requirements for mockup testing of electric systemin piloted aircraft and guided missile

KS W 0631-2004 飞机损伤公差要求

이 규격은 비행기의 비행 안전상 중요한 구조에 대하여 적용하는 손상 허용 설계의 요구

Airplane damage tolerance requirements

KS W 0630-2004 飞机结构完整性程序要求

이 규격의 목적은 비행기 구조 완전성 프로그램 [Aircraft Structural I

Aircraft structural integrity program, airplane requirements

QJ 3201-2004 地（舰）空导弹武器系统“三化”设计指南

Guideline for generalization-seriation design of surface to air missile weapon system

QJ 3198-2004 航天火工装置安全技术要求

Safe technique requirement for pyrotechnic devices used on space vehicles

ISO 15388:2004 空间系统.污染和清洁度控制

This International Standard establishes general requirements for contamination and cleanliness control to be applied, at all tiers of supply, to the development of space systems including ground processing facilities, ground support equipment, launch vehicles, spacecraft, payloads, and ground processing and on-orbit operations. It also provides guidelines for the establishment of a contamination and cleanliness control programme.

Space systems - Contamination and cleanliness control