EN 16603-32-02-2014 航天工程.结构设计及增压硬件的检测.pdf

标准号：EN 16603-32-02-2014
实施状态：现行
中文名称：航天工程.结构设计及增压硬件的检测
英文名称：Space engineering - Structural design and verification of pressurized hardware
发布日期：2014-08
代替标准：FprEN 16603-32-02-2013
采用标准：DIN EN 16603-32-02-2014,IDT;BS EN 16603-32-02-2014,IDT;ECSS-E-ST-32-02C-2008,NEQ;NF L90-300-32-02-2016,IDT;SN EN 16603-32-02-2014,IDT;OENORM EN 16603-32-02-2014,IDTN-EN 16603-32-02-2014,IDT;SS-EN 16603-32-02-2014,IDT;UNE-EN 16603-32-02-2014,IDT;DS/EN 16603-32-02-2014,IDT;UNI CEI EN 16603-32-02:2015-2015,IDT;STN EN 16603-32-02-2015,IDT;CSN EN 16603-32-02-2015,IDT;DS/EN 16603-32-02-2014,IDT;NEN-EN 16603-32-02:2014 en-2014,IDT;SFS-EN 16603-32-02:en-2014,IDT
标准简介：This Standard defines the structural design verification of metallic and non-metallic pressurized hardware which includes pressure vessels, pressurized structures, pressure components (such as valves, pumps, lines, fittings, and hoses), and special pressurized equipment (e.g. batteries, heat pipes, cryostats, sealed containers, hazardous fluids container). External supports and structural interfaces of pressurized hardware are not covered by this standard. Solid propellant motor cases are not covered by this standard. Objectives of the associated verification process are primarily to demonstrate the qualification of design and performance, as meeting all specified requirements, and to ensure that the flight hardware is free from workmanship defects and acceptable for flight. This Standard applies to all space products and in particular to launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, space station, landing probes and rovers, sounding rockets, payloads and instruments. This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.
文件格式：PDF
文件大小：1.49MB
文件页数：80
（以上信息更新时间为：2019-11-28）



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