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Accession Number N14-0003899
Title Recent Progress in Heliogyro Solar Sail Structural Dynamics.
Publication Date Apr 2014
Media Count 8p
Personal Author D. Guerrant E. Dowell J. E. Warren J. N. Juang L. G. Horta S. C. Gibbs W. K. Wilkie
Abstract Results from recent National Aeronautics and Space Administration (NASA) research on the structural dynamics and control characteristics of heliogyro solar sails are summarized. Specific areas under investigation include coupled nonlinear finite element analysis of heliogyro membrane blade with solar radiation pressure effects, system identification of spinning membrane structures, solarelastic stability analysis of heliogyro solar sails, including stability during blade deployment, and results from small-scale in vacuo dynamics experiments with spinning high-aspect ratio membranes. A low-cost, rideshare payload heliogyro technology demonstration mission concept, used as a mission context for these heliogyro structural dynamics and solarelasticity investigations, is also described.
Keywords Degrees of freedom
Dynamic control
Dynamic response
Dynamic structural analysis
Finite element method
High aspect ratio
Low cost
Membrane structures
Membranes
Radiation pressure
Solar sails
Stability tests


 
Source Agency National Aeronautics and Space Administration
NTIS Subject Category 50 - Civil Engineering
84 - Space Technology
Corporate Author National Aeronautics and Space Administration, Hampton, VA. Langley Research Center.
Document Type Conference proceedings
Title Note N/A
NTIS Issue Number 1420
Contract Number N/A

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