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SOLAR SAIL PROPULSION SENSITIVITY TO MEMBRANE SHAPE AND OPTICAL PROPERTIES USING THE SOLAR VECTORING EVALUATION TOOL (SVET)Solar sail propulsive performance is dependent on sail membrane optical properties and on sail membrane shape. Assumptions of an ideal sail (flat, perfect reflector) can result in errors which can affect spacecraft control, trajectory analyses, and overall evaluation of solar sail performance. A MATLAB(R) program has been developed to generate sail shape point cloud files for two square-architecture solar sail designs. Simple parabolic profiles are assumed for sail shape under solar pressure loading. These files are then input into the Solar Vectoring Evaluation Tool (SVET) software to determine the propulsive force vector, center of pressure, and moments about the sail body axes as a function of sail shape and optical properties. Also, the impact of the center-line angle, due to non-perfect optical properties, is addressed since this constrains sail force vector cone angle and is often overlooked when assuming ideal-reflector membranes. Preliminary sensitivity analysis using these tools aids in determining the key geometric and optical parameters that drive solar sail propulsive performance.
Document ID
20060004762
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Ewing, Anthony
(Ewing Research Nashville, TN, United States)
Date Acquired
September 7, 2013
Publication Date
December 7, 2005
Subject Category
Solar Physics
Meeting Information
Meeting: 53rd Joint Army Navy Nasa Air Force (JANNAF) Propulsion Meeting
Location: Monterey, CA
Country: United States
Start Date: December 5, 2005
End Date: December 8, 2005
Funding Number(s)
CONTRACT_GRANT: H35186D
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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