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Recent Progress in Heliogyro Solar Sail Structural DynamicsThe heliogyro is a helicopter-like spinning solar sail concept, conceived by MacNeal in the 1960s and studied by JPL in the 1970s. The heliogyro is a mission-enabling technology:
- Membrane solar sail “blades” are compactly stowed on reels and easily deployed.
- No elaborate management of large, 2-D membranes structures needed, so architecture may be scaled to very large sizes.
- Lightweight due to centrifugal stiffening.

Despite these advantages, development has lagged heavier, square-rigged solar sail designs (e.g., Sunjammer) due to the difficulty of fullscale ground testing. Dynamics need to be validated by (validated) analysis, followed by an affordable flight demonstration, to advance the maturity of heliogyro solar sailing technology.
Document ID
20200007612
Acquisition Source
Langley Research Center
Document Type
Presentation
Authors
Keats Wilkie
(Langley Research Center Hampton, Virginia, United States)
Jay Warren
(Langley Research Center Hampton, Virginia, United States)
Lucas Horta
(Langley Research Center Hampton, Virginia, United States)
Jer-Nan Juang
(Langley Research Center Hampton, Virginia, United States)
Chad Gibbs
(Duke University Durham, North Carolina, United States)
Earl Dowell
(Duke University Durham, North Carolina, United States)
Dan Guerrant
(University of Colorado Boulder Boulder, Colorado, United States)
Dale Lawrence
(University of Colorado Boulder Boulder, Colorado, United States)
Date Acquired
May 14, 2020
Subject Category
Structural Mechanics
Report/Patent Number
Report Number: NF1676L-18560
NF1676L-18560
Meeting Information
Meeting: European Conference on Spacecraft Structures, Materials & Environmental Testing
Location: Braunschweig
Country: DE
Start Date: April 1, 2014
End Date: April 4, 2014
Funding Number(s)
WBS: 432938.02.01.07.43
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
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