Analysis of Pretension and Stress Stiffening in a Self-Deployable Deorbiting Space Structure

Peter Riddersholm Lauridsen, Jan Ánike Nikolajsen, Anders Schmidt Kristensen

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Abstract

In the development of the Self-deployable Deorbiting Space Structure (SDSS) [1][2] FEA are used to determine the stress state during the folding process of a given rectangular Highly Flexible Frame (HFF). The rectangular HFF is the load carrying structure in the SDSS. The stress state changes during the folding process of the HFF and this paper will determine the critical stress states. One of the important subjects in the stowed SDSS is the amount of stored strain energy in the HFF, and the amount of strain energy causes the pretension of the SDSS. To determine the pretension and stress stiffening in a given HFF, non-linear geometrical FEA are conducted.
OriginalsprogEngelsk
TitelProceedings of 7th European Conference on Space Debris
Antal sider4
ForlagEuropean Space Agency
Publikationsdato2017
Artikelnummer1036
StatusUdgivet - 2017
BegivenhedThe 7th European Conference on Space Debris - Darmstadt, Tyskland
Varighed: 18 apr. 201721 apr. 2017
Konferencens nummer: 7

Konference

KonferenceThe 7th European Conference on Space Debris
Nummer7
Land/OmrådeTyskland
ByDarmstadt
Periode18/04/201721/04/2017

Bibliografisk note

Find the paper in folder P-Mitigation

Emneord

  • Space
  • Self-Deployable
  • Stress Stiffening

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