SS-EN-16603-32-03 › Space engineering - Structural finite element models
SS-EN-16603-32-03
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2014 EDITION
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CURRENT
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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, reentry 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.
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Designation Name
SS-EN 16603-32-03:2014
Revision Level
2014 EDITION
Status
Current
Publication Date
Aug. 17, 2014
Language(s)
English
Page Count
32
International Equivalent
EN 16603-32-03:2014(IDT)