Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts

Anders Schmidt Kristensen; Jan Ánike Nikolajsen; Peter Riddersholm Lauridsen

Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts

Anders Schmidt Kristensen, Jan Ánike Nikolajsen, Peter Riddersholm Lauridsen

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

Abstract

A Self-deployable Deorbiting Space Structure (SDSS) is used for drag augmented space debris removal. A highly flexible frame allows for a folding of the structure by bifurcation. This research models the structural loads during the deployment and unfolding of the drag sail in Low Earth Orbit (LEO). The Spacecraft travels with 7.8 km/s at deployment. As the drag sail unfolds instantaneously the structure must withstand the loads from the unfolding and the drag. Thermal loads are included in the FEA as the temperature varies from -80°C to +80°C during deorbit. The results are used to verify the structural integrity, reliability and prepare for approval tests prior to launch.

Originalsprog	Engelsk
Titel	Proceedings of NSCM 30 : The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017
Redaktører	Jan Høgsberg, Niels L. Pedersen
Udgivelsessted	Lyngby
Forlag	DTU Mechanical Engineering
Publikationsdato	2017
Sider	100 -103
Status	Udgivet - 2017
Begivenhed	30th Nordic Seminar on Computational Mechanics - Technical University of Denmark Anker Engelunds Vej 1, Bygning 101A 2800 Kgs. , Lyngby, Danmark Varighed: 25 okt. 2017 → 27 okt. 2017 Konferencens nummer: 30

Konference

Konference	30th Nordic Seminar on Computational Mechanics
Nummer	30
Lokation	Technical University of Denmark Anker Engelunds Vej 1, Bygning 101A 2800 Kgs.
Land/Område	Danmark
By	Lyngby
Periode	25/10/2017 → 27/10/2017

Navn	Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM)
Vol/bind	2017
ISSN	1652-8549

Bibliografisk note

Emneord

Foldable structures
Spacecraft
CubeSat
Dynamic loads
Thermal loads
Applications
Computational Methods
PEEK
Austenitic stainless steel
Aluminum

Adgang til dokumentet

http://3-files.conferencemanager.dk/medialibrary/DEF42602-16D9-4368-83C4-F77E83D08491/images/NSCM_proceedings_23102017.pdf

AUB Link

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Citationsformater

Kristensen, A. S., Nikolajsen, J. Á., & Lauridsen, P. R. (2017). Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts. I J. Høgsberg, & N. L. Pedersen (red.), Proceedings of NSCM 30: The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017 (s. 100 -103). DTU Mechanical Engineering . http://3-files.conferencemanager.dk/medialibrary/DEF42602-16D9-4368-83C4-F77E83D08491/images/NSCM_proceedings_23102017.pdf

Kristensen, Anders Schmidt ; Nikolajsen, Jan Ánike ; Lauridsen, Peter Riddersholm. / Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts. Proceedings of NSCM 30: The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017. red. / Jan Høgsberg ; Niels L. Pedersen. Lyngby : DTU Mechanical Engineering , 2017. s. 100 -103 (Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), Bind 2017).

@inproceedings{efbe85d1bef5469fa29e86e6c8dfb682,

title = "Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts",

abstract = "A Self-deployable Deorbiting Space Structure (SDSS) is used for drag augmented space debris removal. A highly flexible frame allows for a folding of the structure by bifurcation. This research models the structural loads during the deployment and unfolding of the drag sail in Low Earth Orbit (LEO). The Spacecraft travels with 7.8 km/s at deployment. As the drag sail unfolds instantaneously the structure must withstand the loads from the unfolding and the drag. Thermal loads are included in the FEA as the temperature varies from -80°C to +80°C during deorbit. The results are used to verify the structural integrity, reliability and prepare for approval tests prior to launch.",

keywords = "Foldable structures, Spacecraft, CubeSat, Dynamic loads, Thermal loads, Applications, Computational Methods, PEEK, Austenitic stainless steel, Aluminum, Foldable structures, Spacecraft, CubeSat, Dynamic loads, Thermal loads, Applications, Computational Methods, PEEK, Austenitic stainless steel, Aluminum",

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

note = "Copyright {\textcopyright} 2017 by Department of Mechanical Engineering; 30th Nordic Seminar on Computational Mechanics, NSCM30 ; Conference date: 25-10-2017 Through 27-10-2017",

year = "2017",

language = "English",

series = "Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM)",

publisher = "DTU Mechanical Engineering ",

pages = "100 --103",

editor = "Jan H{\o}gsberg and Pedersen, {Niels L.}",

booktitle = "Proceedings of NSCM 30",

}

Kristensen, AS, Nikolajsen, JÁ & Lauridsen, PR 2017, Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts. i J Høgsberg & NL Pedersen (red), Proceedings of NSCM 30: The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017. DTU Mechanical Engineering , Lyngby, Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), bind 2017, s. 100 -103, 30th Nordic Seminar on Computational Mechanics, Lyngby, Danmark, 25/10/2017. <http://3-files.conferencemanager.dk/medialibrary/DEF42602-16D9-4368-83C4-F77E83D08491/images/NSCM_proceedings_23102017.pdf>

Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts. / Kristensen, Anders Schmidt; Nikolajsen, Jan Ánike; Lauridsen, Peter Riddersholm.
Proceedings of NSCM 30: The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017. red. / Jan Høgsberg; Niels L. Pedersen. Lyngby: DTU Mechanical Engineering , 2017. s. 100 -103 (Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), Bind 2017).

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

TY - GEN

T1 - Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts

AU - Kristensen, Anders Schmidt

AU - Nikolajsen, Jan Ánike

AU - Lauridsen, Peter Riddersholm

N1 - Conference code: 30

PY - 2017

Y1 - 2017

N2 - A Self-deployable Deorbiting Space Structure (SDSS) is used for drag augmented space debris removal. A highly flexible frame allows for a folding of the structure by bifurcation. This research models the structural loads during the deployment and unfolding of the drag sail in Low Earth Orbit (LEO). The Spacecraft travels with 7.8 km/s at deployment. As the drag sail unfolds instantaneously the structure must withstand the loads from the unfolding and the drag. Thermal loads are included in the FEA as the temperature varies from -80°C to +80°C during deorbit. The results are used to verify the structural integrity, reliability and prepare for approval tests prior to launch.

AB - A Self-deployable Deorbiting Space Structure (SDSS) is used for drag augmented space debris removal. A highly flexible frame allows for a folding of the structure by bifurcation. This research models the structural loads during the deployment and unfolding of the drag sail in Low Earth Orbit (LEO). The Spacecraft travels with 7.8 km/s at deployment. As the drag sail unfolds instantaneously the structure must withstand the loads from the unfolding and the drag. Thermal loads are included in the FEA as the temperature varies from -80°C to +80°C during deorbit. The results are used to verify the structural integrity, reliability and prepare for approval tests prior to launch.

KW - Foldable structures

KW - Spacecraft

KW - CubeSat

KW - Dynamic loads

KW - Thermal loads

KW - Applications

KW - Computational Methods

KW - PEEK

KW - Austenitic stainless steel

KW - Aluminum

KW - Foldable structures

KW - Spacecraft

KW - CubeSat

KW - Dynamic loads

KW - Thermal loads

KW - Applications

KW - Computational Methods

KW - PEEK

KW - Austenitic stainless steel

KW - Aluminum

M3 - Article in proceeding

T3 - Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM)

SP - 100

EP - 103

BT - Proceedings of NSCM 30

A2 - Høgsberg, Jan

A2 - Pedersen, Niels L.

PB - DTU Mechanical Engineering

CY - Lyngby

T2 - 30th Nordic Seminar on Computational Mechanics

Y2 - 25 October 2017 through 27 October 2017

ER -

Kristensen AS, Nikolajsen JÁ, Lauridsen PR. Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts. I Høgsberg J, Pedersen NL, red., Proceedings of NSCM 30: The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017. Lyngby: DTU Mechanical Engineering . 2017. s. 100 -103. (Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), Bind 2017).

Modelling of Structural Loads in Drag Augmented Space Debris Removal Concepts

Abstract

Konference

Bibliografisk note

Emneord

Adgang til dokumentet

AUB Link

Fingeraftryk

Citationsformater