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

Peter Riddersholm Lauridsen; Jan Ánike Nikolajsen; Anders Schmidt Kristensen

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

Peter Riddersholm Lauridsen, Jan Ánike Nikolajsen, Anders Schmidt Kristensen

Research output: Contribution to book/anthology/report/conference proceeding › Article in proceeding › Research › peer-review

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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.

Original language	English
Title of host publication	Proceedings of 7th European Conference on Space Debris
Number of pages	4
Publisher	European Space Agency
Publication date	2017
Article number	1036
Publication status	Published - 2017
Event	The 7th European Conference on Space Debris - Darmstadt, Germany Duration: 18 Apr 2017 → 21 Apr 2017 Conference number: 7

Conference

Conference	The 7th European Conference on Space Debris
Number	7
Country/Territory	Germany
City	Darmstadt
Period	18/04/2017 → 21/04/2017

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Find the paper in folder P-Mitigation

Keywords

Space
Self-Deployable
Stress Stiffening

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title = "Analysis of Pretension and Stress Stiffening in a Self-Deployable Deorbiting Space Structure",

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.",

keywords = "Space, Self-Deployable, Stress Stiffening, Space, Self-Deployable, Stress Stiffening",

author = "Lauridsen, {Peter Riddersholm} and Nikolajsen, {Jan {\'A}nike} and Kristensen, {Anders Schmidt}",

note = "Find the paper in folder P-Mitigation; The 7th European Conference on Space Debris ; Conference date: 18-04-2017 Through 21-04-2017",

year = "2017",

language = "English",

booktitle = "Proceedings of 7th European Conference on Space Debris",

publisher = "European Space Agency",

}

Analysis of Pretension and Stress Stiffening in a Self-Deployable Deorbiting Space Structure. / Lauridsen, Peter Riddersholm; Nikolajsen, Jan Ánike; Kristensen, Anders Schmidt.
Proceedings of 7th European Conference on Space Debris. European Space Agency, 2017. 1036.

Research output: Contribution to book/anthology/report/conference proceeding › Article in proceeding › Research › peer-review

TY - GEN

T1 - Analysis of Pretension and Stress Stiffening in a Self-Deployable Deorbiting Space Structure

AU - Lauridsen, Peter Riddersholm

AU - Nikolajsen, Jan Ánike

AU - Kristensen, Anders Schmidt

N1 - Conference code: 7

PY - 2017

Y1 - 2017

N2 - 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.

AB - 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.

KW - Space

KW - Self-Deployable

KW - Stress Stiffening

KW - Space

KW - Self-Deployable

KW - Stress Stiffening

UR - https://conference.sdo.esoc.esa.int/proceedings/list

M3 - Article in proceeding

BT - Proceedings of 7th European Conference on Space Debris

PB - European Space Agency

T2 - The 7th European Conference on Space Debris

Y2 - 18 April 2017 through 21 April 2017

ER -

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

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Keywords

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