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Parametric Studies of Square Solar Sails Using Finite Element AnalysisParametric studies are performed on two generic square solar sail designs to identify parameters of interest. The studies are performed on systems-level models of full-scale solar sails, and include geometric nonlinearity and inertia relief, and use a Newton-Raphson scheme to apply sail pre-tensioning and solar pressure. Computational strategies and difficulties encountered during the analyses are also addressed. The purpose of this paper is not to compare the benefits of one sail design over the other. Instead, the results of the parametric studies may be used to identify general response trends, and areas of potential nonlinear structural interactions for future studies. The effects of sail size, sail membrane pre-stress, sail membrane thickness, and boom stiffness on the sail membrane and boom deformations, boom loads, and vibration frequencies are studied. Over the range of parameters studied, the maximum sail deflection and boom deformations are a nonlinear function of the sail properties. In general, the vibration frequencies and modes are closely spaced. For some vibration mode shapes, local deformation patterns that dominate the response are identified. These localized patterns are attributed to the presence of negative stresses in the sail membrane that are artifacts of the assumption of ignoring the effects of wrinkling in the modeling process, and are not believed to be physically meaningful. Over the range of parameters studied, several regions of potential nonlinear modal interaction are identified.
Document ID
20040074322
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Sleight, David W.
(NASA Langley Research Center Hampton, VA, United States)
Muheim, Danniella M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
March 25, 2004
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
AIAA Paper 2004-1509
Report Number: AIAA Paper 2004-1509
Meeting Information
Meeting: 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
Location: Palm Springs, CA
Country: United States
Start Date: April 19, 2004
End Date: April 22, 2004
Sponsors: American Society of Civil Engineers, American Society of Mechanical Engineers, American Inst. of Aeronautics and Astronautics, American Society for Composites, American Helicopter Society, Inc.
Funding Number(s)
OTHER: 755-06-00
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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