V70 航天器综合 标准查询与下载

QJ 20062.2-2011 基于Patran/Nastran软件的航天产品结构有限元分析要求

本部分规定了使用 Patran/Nastran 软件对发射装置进行有限元分析的分析类型，建立发射装置有限 元模型的方法。 本部分适用于使用 Patran/Nastran 软件进行发射装置结构有限元分析、数据及文档管理。使用其他 软件进行有限元分析时可参照执行。

Requirements for Finite Element Analysis of Aerospace Product Structure Based on Patran/Nastran Software

QJ 20062.1-2011 基于Patran/Nastran软件的航天产品结构有限元分析要求

Requirements for Finite Element Analysis of Aerospace Product Structure Based on Patran/Nastran Software

BS ISO 10786:2011 航天系统.结构部件和组件

Space systems. Structural components and assemblies

QJ 20002-2011 月球探测器坐标系

本标准规定了月球探测器的常用坐标系。 本标准适用于月球探测器的设计、研制、发射、飞行控制、测控、空间应用等领域。

Lunar probe coordinate system

QJ 20015-2011 航天器低温表面污染检测方法

本标准规定了真空环境下航天器非金属材料出气污染物在低温表面沉积的检测原理、检测仪器及设备、样品、检测程序、数据处理和检测报告等。 本标准适用于空间环境下航天器用非金属材料出气对低温表面污染沉积的检测。

Test method for contamination on low-temperature surfaces of spacecraft

QJ 20003-2011 航天器磁性检测方法

本标准规定了航天器系统级磁性测试要求，设备、仪器要求和测试方法等。 本标准适用于航天器系统级的磁矩和磁场检测。

Test method for magnetic properties of spacecraft

QJ 1955A-2011 航天器空间环境术语

本标准规定了航天器所遇到空间环境及效应的常用术语和定义。 木标准适用于卫星、飞船、空问站、空间探测器等航天器,也适用于运载火箭。

Terminology for space environment of spacecraft

QJ 20017-2011 航天器真空放电试验方法

本标准规定了航天器真空放电试验的目的、试验要求、试验程序、试验中断及故障处理要求。 本标准适用于航天器在真空环境中可能发生电晕放电和微放电的真空放电试验。

Vacuum discharging test method for spacecraft

BS ISO 24917:2010 空间系统.运载火箭用一般试验要求

Space systems. General test requirements for launch vehicles

ISO 23339:2010 航天系统 无人驾驶飞船 剩余可用推进剂的质量估算

This International Standard gives requirements for estimating the mass of the remaining usable propellant of an unmanned spacecraft in low Earth orbit (LEO) or geostationary Earth orbit (GEO), and for designing propellant measurement systems. It is applicable to spacecraft with either mono- or bi-propellant propulsion systems using liquid or gaseous chemical propellants, and is limited to such systems because they are the most common for spacecraft in LEOs and GEOs.

Space systems - Unmanned spacecraft - Estimating the mass of remaining usable propellant

GJB 7055-2010 地地导弹和运载火箭飞行试验外测弹道综合处理方法

本标准规定了地地导弹和运载火箭飞行试验时外弹道测量数据经预处理后综合解算弹道参数的方法。 本标准适用于地地导弹飞行试验时弹道参数的综合求解，也适用于运载火箭主动段弹道参数的综合求解。对于其他类型试验任务的弹道参数求解也可参照执行。

Synthetic processing method of exterior measuring trajectory for ground-to-ground missile and launch vehicle flight test

GJB 1395A-2009 飞机模拟器通用规范

本规范规定了飞机模拟器的通用要求。 本规范适用于有人驾驶(固定翼)飞机飞行人员训练用飞机模拟器，工程研究用飞机模拟器亦可参照使用。

General specification for airplane simulator

ISO 24638:2008 航天系统.压力部件和压力系统集成

Space systems - Pressure components and pressure system integration

QJ 2841A-2008 弹上电子设备振动控制设计准则与方法

Design criteria and methods for vibration control of missile-mounted electronic equipment

QJ 3293-2008 固体导弹总装测试安全管理要求

Safety management requirements for solid missile final assembly test

QJ 3315-2008 便携式防空导弹武器系统通用规范

General specification for portable anti-aircraft missile weapon system

GJB 6346-2008 军用直升机飞行参数采集要求

本标准规定了军用直升机飞行参数采集的参数数量、采集种类、采集间隔和采集精度等要求。 本标准适用于各类军用直升机。

Requirements for flight date acquisition of military helicopter

GJB 6353-2008 军用直升机系留要求

本标准规定了军用直升机机上系留点和货舱货物系留装置的技术要求及验证。 本标准适用于军用直升机机上系留点和货舱货物系留装置的设计、制造和验证。

Requirements for tie down of military helicopter

QJ 1998A-2007 地（舰）空导弹制导站的精度检飞及评定方法

Accuracy inspection and evaluation method of ground (ship) air missile guidance station

BS ISO 21849:2007 飞行器和太空.工业数据.产品识别和可追溯性

ISO 21849:2006 specifies the requirements for a product identification and traceability schema for life cycle management of aircraft and space products/parts. It specifies the minimum essential identification information needed for traceability of a product for its life cycle. It also provides the data structures for use with automatic identification technologies that support product/part life cycle data management activities. ISO 21849:2006 defines a structure and rules for establishing a unique identifier for product/part identification and traceability. The rules and structure provide sufficient options to support various business practices. They provide the minimum amount of standardization required to support interoperability, improved business processes and efficiency across multiple users and applications of machine-readable media technologies. ISO 21849:2006 also defines and establishes repeatable processes to allow efficient exchange of product data for life cycle product/part traceability, configuration, reliability, maintenance, and product performance management purposes. It specifies the data carriers appropriate for representing the product data in a machine-readable form and associated dimensional and quality parameters. Industries or trading partners will need to develop specific implementation guidelines to employ the principles defined in ISO 21849:2006. Although primarily intended for aircraft and space products/parts, ISO 21849:2006 may be used for other products/parts where desired.

Aircraft and space - Industrial data - Product identification and traceability