标准号：EN 16603-32-03-2014
实施状态：现行
中文名称：航天工程.结构有限元模型
英文名称：Space engineering - Structural finite element models
发布日期：2014-08
代替标准：FprEN 16603-32-03-2013
采用标准：DIN EN 16603-32-03-2014,IDT;BS EN 16603-32-03-2014,IDT;ECSS-E-ST-32-03C-2008,NEQ;NF L90-300-32-03-2016,IDT;SN EN 16603-32-03-2014,IDT;OENORM EN 16603-32-03-2014,IDT;PN-EN 16603-32-03-2014,IDT;SS-EN 16603-32-03-2014,IDT;UNE-EN 16603-32-03-2014,IDT;DS/EN 16603-32-03-2014,IDT;UNI CEI EN 16603-32-03:2015-2015,IDT;STN EN 16603-32-03-2015,IDT;CSN EN 16603-32-03-2015,IDT;DS/EN 16603-32-03-2014,IDT;NEN-EN 16603-32-03:2014 en-2014,IDT;SFS-EN 16603-32-03:en-2014,IDT
标准简介：ECSS-E-ST-32-03 (Space engineering - Structural finite element models) defines the requirements for finite element models used in structural analysis. This Standard specifies the requirements to be met by the finite element models, the checks to be performed and the criteria to be fulfilled, in order to demonstrate model quality. The Standard applies to structural finite element models of space products including: launch vehicles, transfer vehicles, re-entry vehicles, spacecraft, landing probes and rovers, sounding rockets, payloads and instruments, and structural parts of all subsystems. This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
文件格式：PDF
文件大小：1.09MB
文件页数：24
（以上信息更新时间为：2019-11-28）
EN 16603-32-03-2014 航天工程.结构有限元模型.pdf
(1.09 MB)
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