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Normas DIN – AENOR
DIN EN 16603-32-03:2014-10

DIN EN 16603-32-03:2014-10

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

Ingénierie spatiale - Modèles éléments finis pour les structures; Version anglaise EN 16603-32-03:2014

Raumfahrttechnik - Strukturmodelle der finiten Elemente Methode; Englische Fassung EN 16603-32-03:2014

2014-10 /Active
Equivalencias internacionales:

EN 16603-32-03 (2014-08)

Relación con otras normas DIN:
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, re-entry 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.
Aerospace transport, Definitions, Differential equations, Elements, Finite element method, Inspection, Mathematical models, Methods, Methods of calculation, Models, Numeric, Numerical methods, Outer space, Physical, Rockets, Space safety, Space technology, Space transport, Space vehicles, Structure, Testing
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