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Slender solar sail booms: Finite element analysis

Publication ,  Journal Article
Stanciulescu, I; Virgin, LN; Laursen, TA
Published in: Journal of Spacecraft and Rockets
January 1, 2007

Various aspects related to the numerical (finite element) analysis of the support structure for solar sails are analyzed. Static analyses of single booms (simple beam and isogrid configurations) are presented and dynamic properties are extracted before and beyond the buckling load. Numerical difficulties associated with the case of buckling under nonconservative loading are also explored using as a reference example von Beck's problem, for which a closed-form solution for comparison is available. A study of the entire support structure for a square solar sail (four connected booms) is also presented. In all analyses, attention is focused on the prediction of the postbuckling (large deflection) behavior, including dynamics. Copyright © 2007 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.

Duke Scholars

Published In

Journal of Spacecraft and Rockets

DOI

EISSN

1533-6794

ISSN

0022-4650

Publication Date

January 1, 2007

Volume

44

Issue

3

Start / End Page

528 / 537

Related Subject Headings

  • Aerospace & Aeronautics
  • 4001 Aerospace engineering
  • 0913 Mechanical Engineering
  • 0901 Aerospace Engineering
 

Citation

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ICMJE
MLA
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Stanciulescu, I., Virgin, L. N., & Laursen, T. A. (2007). Slender solar sail booms: Finite element analysis. Journal of Spacecraft and Rockets, 44(3), 528–537. https://doi.org/10.2514/1.20526
Stanciulescu, I., L. N. Virgin, and T. A. Laursen. “Slender solar sail booms: Finite element analysis.” Journal of Spacecraft and Rockets 44, no. 3 (January 1, 2007): 528–37. https://doi.org/10.2514/1.20526.
Stanciulescu I, Virgin LN, Laursen TA. Slender solar sail booms: Finite element analysis. Journal of Spacecraft and Rockets. 2007 Jan 1;44(3):528–37.
Stanciulescu, I., et al. “Slender solar sail booms: Finite element analysis.” Journal of Spacecraft and Rockets, vol. 44, no. 3, Jan. 2007, pp. 528–37. Scopus, doi:10.2514/1.20526.
Stanciulescu I, Virgin LN, Laursen TA. Slender solar sail booms: Finite element analysis. Journal of Spacecraft and Rockets. 2007 Jan 1;44(3):528–537.

Published In

Journal of Spacecraft and Rockets

DOI

EISSN

1533-6794

ISSN

0022-4650

Publication Date

January 1, 2007

Volume

44

Issue

3

Start / End Page

528 / 537

Related Subject Headings

  • Aerospace & Aeronautics
  • 4001 Aerospace engineering
  • 0913 Mechanical Engineering
  • 0901 Aerospace Engineering