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

BS EN 16603-32-03:2014

Space engineering. Structural finite element models

Status : Current   Published : August 2014

Format
PDF

Format
HARDCOPY



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.




Standard NumberBS EN 16603-32-03:2014
TitleSpace engineering. Structural finite element models
StatusCurrent
Publication Date31 August 2014
Normative References(Required to achieve compliance to this standard)EN 16601-00-01, EN 16603-32, ECSS-S-ST-00-01, ECSS-E-ST-32
Informative References(Provided for Information)EN 16601-00, EN 16603-32-11, ECSS-S-ST-00, ECSS-E-ST-32-11
International RelationshipsEN 16603-32-03:2014
DescriptorsAir safety, Space safety, Air transport, Aerospace transport, Test models, Mathematical calculations
ICS49.140
Title in FrenchIngénierie spatiale. Modèles éléments finis pour les structures
Title in GermanRaumfahrttechnik. Strukturmodelle der finiten Elemente Methode
CommitteeACE/68
ISBN978 0 580 83983 2
PublisherBSI
FormatA4
DeliveryYes
Pages24
File Size1.057 MB
Price£182.00


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