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

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Resumé

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.
OriginalsprogEngelsk
TitelProceedings of 7th European Conference on Space Debris
Antal sider6
ForlagEuropean Space Agency
Publikationsdato2017
Artikelnummer1041
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
LandTyskland
ByDarmstadt
Periode18/04/201721/04/2017

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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.",
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Nikolajsen, JÁ, Lauridsen, PR & Kristensen, AS 2017, Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures. i Proceedings of 7th European Conference on Space Debris., 1041, European Space Agency, Darmstadt, Tyskland, 18/04/2017.

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 proceedingKonferenceartikel i proceedingForskningpeer review

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AU - Lauridsen, Peter Riddersholm

AU - Kristensen, Anders Schmidt

N1 - Find the paper in folder P-Mitigation

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

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BT - Proceedings of 7th European Conference on Space Debris

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Nikolajsen JÁ, Lauridsen PR, Kristensen AS. Modelling and Analysis of the Folding Principle used in Selv-Deployable Deorbiting Space Structures. I Proceedings of 7th European Conference on Space Debris. European Space Agency. 2017. 1041