Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures

Jan Ánike Nikolajsen; Peter Riddersholm Lauridsen; Anders Schmidt Kristensen

Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures

Jan Ánike Nikolajsen, Peter Riddersholm Lauridsen, Anders Schmidt Kristensen

Publikation: Bidrag til bog/antologi/rapport/konference proceeding › Konferenceartikel i proceeding › Forskning › peer review

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Abstract

An initial prototype of the Self-deployable Deorbiting Space Structure (SDSS) for semi-controlled debris removal was launched in 2014. The SDSS module consists of 3 main systems, i.e. the Drag Sail Unit (DSU), the Release Unit (RU) and the Housing Unit (HU). In the redesign, a storage lid is introduced whereby the folded drag sail is completely separated from the HU during the release process. During the research, an updated version of the SDSS version is made for CubeSat. The prototype is for a CubeSat which will be scalable.

Originalsprog	Engelsk
Titel	Proceedings of 7th European Conference on Space Debris
Antal sider	6
Forlag	European Space Agency
Publikationsdato	2017
Artikelnummer	1041
Status	Udgivet - 2017
Begivenhed	The 7th European Conference on Space Debris - Darmstadt, Tyskland Varighed: 18 apr. 2017 → 21 apr. 2017 Konferencens nummer: 7

Konference

Konference	The 7th European Conference on Space Debris
Nummer	7
Land/Område	Tyskland
By	Darmstadt
Periode	18/04/2017 → 21/04/2017

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title = "Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures",

abstract = "An initial prototype of the Self-deployable Deorbiting Space Structure (SDSS) for semi-controlled debris removal was launched in 2014. The SDSS module consists of 3 main systems, i.e. the Drag Sail Unit (DSU), the Release Unit (RU) and the Housing Unit (HU). In the redesign, a storage lid is introduced whereby the folded drag sail is completely separated from the HU during the release process. During the research, an updated version of the SDSS version is made for CubeSat. The prototype is for a CubeSat which will be scalable.",

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

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Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures. / Nikolajsen, Jan Ánike; Lauridsen, Peter Riddersholm; Kristensen, Anders Schmidt.
Proceedings of 7th European Conference on Space Debris. European Space Agency, 2017. 1041.

Publikation: Bidrag til bog/antologi/rapport/konference proceeding › Konferenceartikel i proceeding › Forskning › peer review

TY - GEN

T1 - Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures

AU - Nikolajsen, Jan Ánike

AU - Lauridsen, Peter Riddersholm

AU - Kristensen, Anders Schmidt

N1 - Conference code: 7

PY - 2017

Y1 - 2017

N2 - An initial prototype of the Self-deployable Deorbiting Space Structure (SDSS) for semi-controlled debris removal was launched in 2014. The SDSS module consists of 3 main systems, i.e. the Drag Sail Unit (DSU), the Release Unit (RU) and the Housing Unit (HU). In the redesign, a storage lid is introduced whereby the folded drag sail is completely separated from the HU during the release process. During the research, an updated version of the SDSS version is made for CubeSat. The prototype is for a CubeSat which will be scalable.

AB - An initial prototype of the Self-deployable Deorbiting Space Structure (SDSS) for semi-controlled debris removal was launched in 2014. The SDSS module consists of 3 main systems, i.e. the Drag Sail Unit (DSU), the Release Unit (RU) and the Housing Unit (HU). In the redesign, a storage lid is introduced whereby the folded drag sail is completely separated from the HU during the release process. During the research, an updated version of the SDSS version is made for CubeSat. The prototype is for a CubeSat which will be scalable.

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 -

Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures

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