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EN 16603-32-03:2014

Current

Current

The latest, up-to-date edition.

Space engineering - Structural finite element models

Published date

13-08-2014

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Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions, and
  abbreviated terms
4 General requirements
5 Model checks
6 Test - Analysis correlation
Bibliography

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.

Committee
CEN/CLC/JTC 5
DocumentType
Standard
ProductNote
This standard identical to ECSS-E-ST-32-03C
PublisherName
Comite Europeen de Normalisation
Status
Current

BS EN 16603-32:2014 Space engineering. Structural general requirements
EN 16603-32:2014 Space engineering - Structural general requirements
I.S. EN 16603-32:2014 SPACE ENGINEERING - STRUCTURAL GENERAL REQUIREMENTS

EN 16603-32-11:2014 Space engineering - Modal survey assessment
EN 16601-00-01:2015 Space systems - Glossary of terms
EN 16603-32:2014 Space engineering - Structural general requirements

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