V72 航天器动力系统 标准查询与下载

DIN EN 14607-5-1:2006 航天工程. 机械. 第5-1部分: 航天器液体和电力推进器; 英文版本EN 14607-5-1: 2004

Thie Part 5-1 of space engineering - mechanical defined the requirements for the discipline liquid and electric propulsion for spacecraft.

Space engineering - Mechanical - Part 5-1: Liquid and electric propulsion for spacecraft; English version EN 14607-5-1:2004

CISPR 20-2006 飞行器燃料舱中用作爆炸抑制剂和挡板材料的纤维聚酰胺材料.试验方法

Sound and television broadcast receivers and associated equipment - Immunity characteristics - Limits and methods of measurement

CISPR 16-1-2 Edition 1.2-2006 无线电干扰和抗扰度测量设备和方法规范. 第1-2部分: 无线电干扰和抗扰度测量设备. 辅助设备. 传导干扰

This part of CISPR 16 is designated a basic standard, which specifies the characteristics and performance of equipment for the measurement of radio disturbance voltages and currents in the frequency range 9 kHz to 1 GHz.

Specification for radio disturbance and immunity measuring apparatus and methods.Part 1-2: Radio disturbance and immunity measuring apparatus – Ancillary equipment – Conducted disturbances

GJB 5584-2006 电子式火箭控制盒通用规范

本规范规定了航空火箭发射器中安装的电子式火箭控制盒（以下简称控制盒）的通用要求。 本规范适用于控制盒的设计、制造、检验及验收。

General specification for electronic aircraft rocket firing unit

QJ 1044A-2005 可贮存推进剂液体火箭发动机试验方法

Test methods for storable propellant liquid rocket motors

GJB 1546A-2005 小推力液体火箭推进系统通用规范

本规范规定了小推力液体火箭推进系统的技术要求、质量保证规定和交货准备。 本规范适用于导弹和运载火箭用小推力液体火箭推进系统(以下简称推进系统)的研制、生产和验收。

General specification for low thrust liquid rocket propulsion system

GJB 1025A-2005 固体火箭发动机直径系列

本标准规定了固体火箭发动机的直径系列。 本标准适用于导弹、运载火箭、航天器及火箭弹用的固体火箭发动机。

A series for diameters of solid rocket motors

GJB/J 5458-2005 固体推进剂靶线法燃速仪检定规程

本检定规程规定了固体推进剂靶线法燃速仪（以下简称燃速仪）的检定技术要求、检定条件、检定项目、检定方法和检定结果的处理和检定周期。 本检定规程适用于新制造、使用中和修理后的燃速仪的检定。

Verificationg regulation for burning instrument of target line method of solid propellants

GJB 5420-2005 固体火箭发动机跌落试验方法

本标准规定了固体火箭发动机跌落试验的条件、设备、程序、结果评定方法和报告内容等。 本标准适用于固体火箭发动机（以下简称发动机）跌落试验。

Fall off test method for solid rocket motor

QJ 1492A-2005 液体火箭发动机试验数据处理方法

本标准规定了液体火箭发动机试验的数据处理准备、处理方法和试验结果报告的编制。 本标准适用于液体火箭发动机地面试验稳态参数数据处理。

Data process method for liquid rocket engine test

GJB 1184A-2005 航空机轮和刹车装置通用规范

本规范规定了航空机轮和刹车装置的设计、制造要求以及质量保证规定。 本规范适用于军用飞机的前轮(尾轮)、主轮、辅助轮以及刹车装置的设计、制造和验收。直升机可参照执行。

General specification for aircraft wheel and brake assemblies

CISPR 16-2-3 AMD 2-2005 飞行器燃料舱中用作爆炸抑制剂和挡板材料的纤维聚酰胺材料.试验方法

This standard is Amendment 2 Specification for radio disturbance and immunity measuring apparatus and methods-Part 2-3:Methods of measurement of disturbances and immunity-Radiated disturbance measurements

Amendment 2 Specification for radio disturbance and immunity measuring apparatus and methods-Part 2-3:Methods of measurement of disturbances and immunity-Radiated disturbance measurements

CISPR 16-3 AMD 1-2005 飞行器燃料舱中用作爆炸抑制剂和挡板材料的纤维聚酰胺材料.试验方法

This standard is Amendment 1 Specification for radio disturbance and immunity measuring apparatus and methods-Part 3:CISPR technical reports

Amendment 1 Specification for radio disturbance and immunity measuring apparatus and methods-Part 3:CISPR technical reports

CISPR 16-2-1 AMD 1-2005 飞行器燃料舱中用作爆炸抑制剂和挡板材料的纤维聚酰胺材料.试验方法

Amendment 1 Specification for radio disturbance and immunity measuring apparatus and methods-Part 2-1:Methods of measurement of disturbances and immunity-Conducted disturbance measurements

CISPR 16-1-1 AMD 1-2005 飞行器燃料舱中用作爆炸抑制剂和挡板材料的纤维聚酰胺材料.试验方法

This standard is Amendment 1 Specification for radio disturbance and immunity measuring apparatus and methods-Part 1-1:Radio disturbance and immunity measuring apparatus-Measuring apparatus

Amendment 1 Specification for radio disturbance and immunity measuring apparatus and methods-Part 1-1:Radio disturbance and immunity measuring apparatus-Measuring apparatus

BS EN 14607-6:2005 航天工程.机械.信号弹

Space engineering - Mechanical - Pyrotechnics

BS EN 14607-6:2004 航天工程.机械.信号弹

EN 14607 Part 6 of Space engineering - Mechanical defines the requirements for the discipline of pyrotechnics engineering. This part defines the standards to be applied for the use of pyrotechnics on all spacecraft and other space products including launch vehicles. It addresses the aspects of design, analysis, verification, manufacturing, operations and safety. As any pyrotechnic item used for flight can function only once, it can never be fully tested before its crucial mission operation. The required confidence can only be established indirectly by the testing of identical items. Test results and theoretical justification are essential for demonstration of fulfilment of the requirements. The requirement for repeatability shows that product assurance plays a crucial role in support of technical aspects. The failure or unintentional operation of a pyrotechnic item can be catastrophic for the whole mission and life threatening. Specific requirements can exist for the items associated with it. As all pyrotechnic functions are to be treated similarly, collective control needs to be applied in the manner of a subsystem. 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 6:Pyrotechnics

BS EN 14607-5-1:2005 航天工程.机械.航天器液体和电力推进器

Space engineering - Mechanical - Liquid and electric propulsion for spacecraft

BS EN 14607-5-1:2004 航天工程.机械.航天器液体和电力推进器

EN 14607 Part 5.1 of Space engineering - Mechanical defined the requirements for the discipline liquid and electric propulsion for spacecraft This document belongs to the propulsion field of the mechanical discipline, as defined in EN 13292, and defines the regulatory aspects applicable to elements and processes for liquid, including cold gas, and electrical propulsion for spacecraft. It specifies the activities to perform in the engineering of such propulsion systems, their applicability, and defines the requirements for the engineering aspects: functional, configurational, interfaces, physical, environmental, quality factors, operational and verification. General requirements relating to Mechanical Engineering are defined in EN 14607 Part 1. This document applies only to liquid, including cold gas, and electrical propulsion systems used in spacecraft and to related mechanical parts. Solid propulsion for spacecraft, and solid and liquid propulsion for launchers are not covered by this document. Other forms of propulsion currently under development (e.g. nuclear, nuclear-electric, solar-thermal and hybrid propulsion) are not presently covered by this document. When viewed in 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 5-1:Liquid and electric propulsion for spacecraft

GJB 5400-2005 氢氧火箭发动机阀门用金属波纹管规范

本规范规定了氢氧火箭发动机阀门用金属波纹管（以下简称波纹管）的要求、质量保证规定、交货准备等。 本规范适用于波纹管的试制、制造、检验与验收。

Specification for valve metal bellows of hydrogen-oxygen rocket engine