EN 16603-32-03:2014

Space engineering - Structural finite element models EN 16603-32-03:2014

Publication date:   Nov 17, 2014

General information

90.93   Standard confirmed   Jul 27, 2022

CEN/CENELEC

CEN/CLC/JTC 5 Space

European Norm

49.140   Space systems and operations

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Scope

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.

Life cycle

NOW

PUBLISHED
EN 16603-32-03:2014
90.93 Standard confirmed
Jul 27, 2022

Relations

Adopted from ECSS-E-ST-32-03C IDENTICAL




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