BS EN 16603-32-03:2014
Current
The latest, up-to-date edition.
Space engineering. Structural finite element models
Hardcopy , PDF
English
31-08-2014
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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