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BS EN 16603-32-03:2014

Current

Current

The latest, up-to-date edition.

Space engineering. Structural finite element models

Available format(s)

Hardcopy , PDF

Language(s)

English

Published date

31-08-2014

€217.36
Excluding VAT

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

Describes the requirements for finite element models used in structural analysis.

Committee
ACE/68
DocumentType
Standard
Pages
24
PublisherName
British Standards Institution
Status
Current

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.

Standards Relationship
EN 16603-32-03:2014 Identical

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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