Development of a Validated FE Model of the SIMOD Structure.

Hermes, M. (1996) Development of a Validated FE Model of the SIMOD Structure. DLR-Interner Bericht. IB 232 - J 01. 73 S.

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Abstract

Vibrations are a major problem for all spacecraft during their launching period. In order to develop and demonstrate advanced methods for structure qualification to solve these problems, a joint project with the Canadian Space Agency (CSA) was initiated. The aim of this project is to predict the dynamic behaviour of a test structure because of the known dynamic behaviour of its substructures. For this prediction, an FE model of the test structurewill be created, consisting of validated FE models of the substructures. This report summarizes the development, validation, and updating of the FE model of one of the substructures.

Item URL in elib:

https://elib.dlr.de/39765/

Document Type:

Monograph (DLR-Interner Bericht)

Additional Information:

LIDO-Berichtsjahr=1996,

Title:

Development of a Validated FE Model of the SIMOD Structure.

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Hermes, M.	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED

Date:

1996

Open Access:

Gold Open Access:

In SCOPUS:

In ISI Web of Science:

Number of Pages:

Status:

Published

Keywords:

simple model of a satellite structure, modal survey test, modal updating, dynamic Finite Element Analysis

HGF - Research field:

UNSPECIFIED

HGF - Program:

Space (old)

HGF - Program Themes:

W RP - Raumtransport

DLR - Research area:

UNSPECIFIED

DLR - Program:

W RP - Raumtransport

DLR - Research theme (Project):

UNSPECIFIED

Location:

Göttingen

Institutes and Institutions:

Institute of Aeroelasticity

Deposited By:

DLR-Beauftragter, elib

Deposited On:

02 Apr 2006

Last Modified:

27 Apr 2009 10:53

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