TECHNICAL PAPERS
Oct 1, 1995

Simplified Design Method for Braced Double-Skinned Structure in Lunar Application

Publication: Journal of Aerospace Engineering
Volume 8, Issue 4

Abstract

A simplified design methodology is developed for the preliminary design of a proposed braced double-skinned roof structure for lunar applications, using Navier's and Levy's plate solutions. A finite-element analysis of the structure is performed to evaluate the accuracy of the design methodology. Results from extensive parametric studies are used to select the final dimensions of the braced double-skinned roof assembly for realistic static loading. The natural frequencies of the proposed roof structure are evaluated by a simplified relation and are compared with those obtained by the finite-element method.

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References

1.
Adib-Jahromi, H., Malla, R., and Accorsi, M. (1994). “Braced double-skinned structure in lunar applications.”Proc., SPACE 94 Conf., R. Galloway and S. Lokaj, eds., ASCE, New York, N.Y. 47–56.
2.
ASCE Task Committee on Lunar Base Structures.(1992). “Overview of existing lunar base structural concepts.”J. Aerosp. Engrg., ASCE, 5(2), 159–174.
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Information & Authors

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Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 8Issue 4October 1995
Pages: 189 - 195

History

Published online: Oct 1, 1995
Published in print: Oct 1995

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Authors

Affiliations

Ramesh B. Malla
Asst. Prof., Dept. of Civ. and Envir. Engrg., U-37, Univ. of Connecticut, Storrs, CT 06269.
Hamid R. Adib-Jahromi
Proj. Mgr., BVH Engineers Inc., Bloomfield, CT 06002; formerly, PhD Candidate, Dept. of Civ. and Envir. Engrg., Univ. of Connecticut, CT 06269.
Michael L. Accorsi
Assoc. Prof., Dept. of Civ. and Envir. Engrg., Univ. of Connecticut, Storrs, CT.

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