V71 航天器总体 标准查询与下载

GJB 2499A-2006 包带弹簧式星箭连接分离装置通用规范

本规范规定了包带弹簧式星箭连接分离装置的结构形式、技术要求、质量保证规定、交货准备等。 本规范适用于包带弹簧式星箭连接分离装置（以下简称装置）的设计、生产、试验、交货、验收。航天器上用的包带弹簧式连接分离装置亦可参照使用。

General specifIcation for clampband4pring satellite-launcher release device

GJB 5894-2006 火箭破障弹综合破障模拟试验方法

本标准规定了火箭破障弹（以下简称被试品）综合破障模拟试验原理、试验装置、设备、被试品状态、试验条件、试验程序、试验数据录取和处理等要求。 本标准适用于毁伤目标为轨条岩的火箭破障弹综合破障模拟试验，其他类似产品可参照执行。

Simulated test method of integrated obstacle sweeping of rocket

BS ISO 15863:2006 航天系统.航天飞机与运载工具间接口的控制文献

The purpose of this International Standard is to provide spacecraft (SC) and launch vehicle (LV) organizations with the general format for presenting the interface control document (ICD) that verifies and controls the compatibility between SC and LV for a dedicated mission. This International Standard addresses the definition of the mission, the compatibility of the SC with the LV environment, including all mechanical, electrical, radio frequency, and electromagnetic aspects related to SC to LV and SC to launch range interfaces, verification analyses and tests for the induced environment, and the necessary facilities and support for launch range operations.

Space systems - Spacecraft-to-launch-vehicle interface control document

ASTM F2564-06 轻型运动滑翔机设计和性能标准规范

1.1 This specification covers airworthiness requirements for the design of a powered or non-powered fixed wing light sport aircraft, a "glider." 1.2 This specification is applicable to the design of a light sport aircraft glider as defined by regulations and limited to day VFR flight.1.3 A glider for the purposes of this specification is defined as a heavier than air aircraft that remains airborne through the dynamic reaction of the air with a fixed wing and in which the ability to remain aloft in free flight does not depend on the propulsion from a power plant. A powered glider is defined for the purposes of this specification as a glider equipped with a power plant in which the flight characteristics are those of a glider when the power plant is not in operation.1.4 The values in SI units are to be regarded as the standard. The values in parenthesis are for information only.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 requirements prior to use.

Standard Specification for Design and Performance of a Light Sport Glider

GJB 1414A-2005 战术导弹贮运发射箱（筒）通用规范

本规范规定了战术导弹贮运发射箱(筒)技术要求、质量保证规定和交货准备。 本规范适用于战术导弹不同类型的贮运发射箱(筒)(以下简称“发射箱”)的设计、制造也验收，也适用于其它飞行器的发射箱。

General specification for the storage-transport launch container of tactical missiles

GJB 1492A-2005 高破片率弹体用钢棒规范

本规范规定了高破片率弹体用钢棒的要求、质量保证规定及交货准备等。 本规范适用于高破片率弹体用圆钢和方钢。

Specification for steel bar for projectile of high-broken pieces

GJB 2203A-2005 卫星产品洁净度及污染控制要求

本标准规定了卫星产品(以下简称“产品”)的洁净度等级分类、产品和环境的洁净度要求，以及产品设计、生产、试验、运输、贮存和发射准各过程中污染控制的一般要求和方法。 本标准适用于卫星产品设计、生产、试验过程中与污染控制有关的产品质量控制。其它航天器、产品测试设备、试验设施和洁净度有控环境等可参照使用。

Cleanliness and contamination control requirements for satellite product

GJB 4013A-2005 氢氧三级运载火箭测试发射规程

本标准规定了带氢氧级的三级运载火箭(CZ-3A、CZ-3B、CZ-3C等，以下简称火箭)在发射中心的测试、运输、吊装、加注、发射等工作程序和有关技术要求。 本标准适用于火箭在发射中心的测试发射，火箭在发射中心的合练亦可参照执行。

Testing and launching rules for three-stage rocket of LOX/LH engine

BS EN 14607-7:2004 航天工程.机械.机械部件

EN 14607 Part 7 of Space engineering - Mechanical defines the mechanical engineering requirements for mechanical parts. This document defines the requirements applicable to the selection, design, verification and application of mechanical parts to promote the use of high-quality non-critical mechanical parts that achieve robust functionality and satisfy the mission performance requirements. This document defines a pragmatic approach to the selection of parts by the mechanical and design engineer on the basis of their effect on the integrity of the equipment and to streamline the selection of space-proven rather than non space-proven parts during the design of a new equipment in order to select the least number of different parts to satisfy the mission requirements. It defines performance, design, test, product assurance and support activity requirements for the use of mechanical parts in space applications. 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.

Space engineering-Mechanical-Part 7:Mechanical parts

BS EN 14607-2:2005 航天工程.机械.结构

Space engineering - Mechanical - Structural

BS EN 14607-8:2004 航天工程.机械.材料

EN 14607 Part 8 of Space engineering - Mechanical defines the mechanical engineering requirements for materials. This document also encompasses the effects of the natural and induced environments to which materials used for space applications can be subjected. This document defines requirements for the establishment of the required mechanical and physical properties of the materials including the effects of the environmental conditions, material selection, procurement, production and verification. Verification includes destructive and non-destructive test methods. Material procurement and control is closely related to required quality assurance procedures and detailed references to EN 13291-3 are made. 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.

Space engineering-Mechanical-Part 8:Materials

BS EN 14607-2:2004 航天工程.机械.结构

Part 2 of Space engineering - Mechanical defines the mechanical engineering requirements for structural engineering. This document specifies the requirements to consider in all engineering aspects of structures: requirement definition and specification, design, development, verification, production, in-service and eventual disposal. The document applies to all general structural subsystem aspects of space including: launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems. 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.

Space engineering Mechanical-Part 2:Structural

BS EN 14607-8:2005 航天工程.机械.材料

Space engineering - Mechanical - Materials

QJ 3204-2005 战略导弹弹头综合离心试验方法

本标准规定了战略导弹弹头综合离心试验的依据、目的、要求、加载、程序、测量项目与要求和结果评定。 本标准适用于战略导弹弹头（以下简称弹头）的综合离心试验。

Compositive centrifuge test method for strategic missle warhead

QJ 3206-2005 导弹全胶接复合材料弹翼通用规范

本规范规定了导弹全胶接复合材料弹簧的技术要求、质量保证规定和交货准备。 本规范适用于导弹全胶接碳纤维复合材料弹簧（以下简称弹簧）的生产与验收。尾翼中的全胶接碳纤维复合材料外翼与驼面等也可参照执行。

General specifications for full adhesive composite wing of missile

QJ 3209-2005 YS2型深水圆形电连接器详细规范

本规范规定了YS2型深水圆形电连接器（以下简称电连接器）的技术要求、质量保证规定和交货准备。 本规范适用于电连接器的生产、验收及产品交付。

Detail specification for YS2 connertors, electrical,circular,under-deep-water

QJ 3210-2005 JXZ型小型三向阻尼隔振器规范

本规范规定了JXZ型小型三向阻尼隔振器的技术要求、质量保证规定和交货准备。 本规范适用于弹上与箭上电子、电气设备及其他设备使用的JXZ型小型三向阻尼隔振器（以下简称隔振器）的生产、验收、使用。

Specification for JXZ type miniaturized three-dimensional damping isolator

QJ 3213-2005 航天产品维修性设计与验证指南

本指导性技术文件提供了航天产品维修性设计与验证的工作内容和方法，并给出了维修性的设计准则及验证应用示例。 本指导性技术文件中的相关要求与技术内容适用于各类航天产品研制的各阶段。

Guideline of maintainability design and demonstration for space products

QJ 2172A-2005 卫星可靠性设计指南

本标准规定了卫星系统、分系统及设备可靠性设计和分析方法。 本标准适用于卫星系统、分系统及设备的可靠性设计，卫星地面设备及其它航天器可参照执行。

Guide to satellite reliability design

QJ 3220-2005 飞航导弹虚拟样机结构件建模要求

本标准规定了Unigraphics(以下简称UG)NX软件进行飞航导弹弹体结构设计的造型原则和建模方法。 本标准适用于以UG NX软件(及后续版本）进行飞航导弹虚拟样机结构件的建模、其它设备结构件的建模可参照执行。

The modeling requiremnt for structuring parts of the winged missile's virtual prototype