Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites

Publikation: Bidrag til bog/antologi/rapport/konference proceedingKonferenceartikel i proceedingForskningpeer review

Resumé

Structural analysis of a sail solution1 to deorbit satellites is presented in this paper. The deployable drag sail consists of a circular highly flexible frame, sail and housing. The folding process of the highly flexible frame is complex and is only possible to describe analytical2 without a sail attached to the highly flexible frame. FEA has shown a significant difference in the structural behavior with a sail attached to the highly flexible frame and this paper will present these results. Stresses, moment reactions and kinematics are compared in two system (e.g. with and without a drag sail attached to the highly flexible frame). Simulation of folding a drag sail can be challenging due to the instability and slenderness of the structure.
OriginalsprogEngelsk
TitelProceedings of NSCM 30 : The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017
RedaktørerJan Høgsberg, Niels L. Pedersen
Udgivelses stedLyngby
ForlagDTU Mechanical Engineering
Publikationsdato2017
Sider114-117
StatusUdgivet - 2017
Begivenhed30th Nordic Seminar on Computational Mechanics - Technical University of Denmark Anker Engelunds Vej 1, Bygning 101A 2800 Kgs. , Lyngby, Danmark
Varighed: 25 okt. 201727 okt. 2017
Konferencens nummer: 30

Konference

Konference30th Nordic Seminar on Computational Mechanics
Nummer30
LokationTechnical University of Denmark Anker Engelunds Vej 1, Bygning 101A 2800 Kgs.
LandDanmark
ByLyngby
Periode25/10/201727/10/2017
NavnProceedings of the Nordic Seminar on Computational Mechanics, (NSCM)
Vol/bind2017
ISSN1652-8549

Fingerprint

Structural analysis
Drag
Satellites
Kinematics
Finite element method

Bibliografisk note

Copyright © 2017 by Department of Mechanical Engineering

Emneord

  • Space Debris
  • Deployable Systems
  • Non-Linear Geometric Effects
  • FEA
  • Slenderness
  • Structural Analysis

Citer dette

Lauridsen, P. R., Nikolajsen, J. Á., & Kristensen, A. S. (2017). Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites. I J. Høgsberg, & N. L. Pedersen (red.), Proceedings of NSCM 30: The 30th Nordic Seminar on Computational Mechanics 25-27 October 2017 (s. 114-117). Lyngby: DTU Mechanical Engineering . Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), Bind. 2017
Lauridsen, Peter Riddersholm ; Nikolajsen, Jan Ánike ; Kristensen, Anders Schmidt. / Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites. 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. 114-117 (Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), Bind 2017).
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title = "Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites",
abstract = "Structural analysis of a sail solution1 to deorbit satellites is presented in this paper. The deployable drag sail consists of a circular highly flexible frame, sail and housing. The folding process of the highly flexible frame is complex and is only possible to describe analytical2 without a sail attached to the highly flexible frame. FEA has shown a significant difference in the structural behavior with a sail attached to the highly flexible frame and this paper will present these results. Stresses, moment reactions and kinematics are compared in two system (e.g. with and without a drag sail attached to the highly flexible frame). Simulation of folding a drag sail can be challenging due to the instability and slenderness of the structure.",
keywords = "Space Debris, Deployable Systems, Non-Linear Geometric Effects, FEA, Slenderness, Structural Analysis, Space Debris, Deployable Systems, Non-Linear Geometric Effects, FEA, Slenderness, Structural Analysis",
author = "Lauridsen, {Peter Riddersholm} and Nikolajsen, {Jan {\'A}nike} and Kristensen, {Anders Schmidt}",
note = "Copyright {\circledC} 2017 by Department of Mechanical Engineering",
year = "2017",
language = "English",
pages = "114--117",
editor = "Jan H{\o}gsberg and Pedersen, {Niels L.}",
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Lauridsen, PR, Nikolajsen, JÁ & Kristensen, AS 2017, Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites. 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. 114-117, Lyngby, Danmark, 25/10/2017.

Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites. / Lauridsen, Peter Riddersholm; Nikolajsen, Jan Ánike; Kristensen, Anders Schmidt.

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. 114-117.

Publikation: Bidrag til bog/antologi/rapport/konference proceedingKonferenceartikel i proceedingForskningpeer review

TY - GEN

T1 - Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites

AU - Lauridsen, Peter Riddersholm

AU - Nikolajsen, Jan Ánike

AU - Kristensen, Anders Schmidt

N1 - Copyright © 2017 by Department of Mechanical Engineering

PY - 2017

Y1 - 2017

N2 - Structural analysis of a sail solution1 to deorbit satellites is presented in this paper. The deployable drag sail consists of a circular highly flexible frame, sail and housing. The folding process of the highly flexible frame is complex and is only possible to describe analytical2 without a sail attached to the highly flexible frame. FEA has shown a significant difference in the structural behavior with a sail attached to the highly flexible frame and this paper will present these results. Stresses, moment reactions and kinematics are compared in two system (e.g. with and without a drag sail attached to the highly flexible frame). Simulation of folding a drag sail can be challenging due to the instability and slenderness of the structure.

AB - Structural analysis of a sail solution1 to deorbit satellites is presented in this paper. The deployable drag sail consists of a circular highly flexible frame, sail and housing. The folding process of the highly flexible frame is complex and is only possible to describe analytical2 without a sail attached to the highly flexible frame. FEA has shown a significant difference in the structural behavior with a sail attached to the highly flexible frame and this paper will present these results. Stresses, moment reactions and kinematics are compared in two system (e.g. with and without a drag sail attached to the highly flexible frame). Simulation of folding a drag sail can be challenging due to the instability and slenderness of the structure.

KW - Space Debris

KW - Deployable Systems

KW - Non-Linear Geometric Effects

KW - FEA

KW - Slenderness

KW - Structural Analysis

KW - Space Debris

KW - Deployable Systems

KW - Non-Linear Geometric Effects

KW - FEA

KW - Slenderness

KW - Structural Analysis

M3 - Article in proceeding

SP - 114

EP - 117

BT - Proceedings of NSCM 30

A2 - Høgsberg, Jan

A2 - Pedersen, Niels L.

PB - DTU Mechanical Engineering

CY - Lyngby

ER -

Lauridsen PR, Nikolajsen JÁ, Kristensen AS. Non-linear Structural Analysis of the Folding Process in a Deployable System for Satellites. 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. 114-117. (Proceedings of the Nordic Seminar on Computational Mechanics, (NSCM), Bind 2017).