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Segmented Hexagonal Antenna Reflector Concentrically Stacked Using Shape Memory Composite Tubular HingesA new architecture for solid surface reflector antennas scalable to sizes greater than 10 m is presented. The design combines the compact, lightness and simplicity characteristics of advanced deployable structures to create sub-reflectors that can be assembled in space into larger units using a robotic arm and operations under development by a related parallel project. The seven-panel hexagonal sub-reflector is divided into hexagonal panels of that efficiently stack concentrically and vertically. The central panel is connected to each side panel on the back side by a pair of tubular shape memory composite hinges that enable the required deployment kinematics. A secondary mechanism ultimately closes the interpanel gap. The focus of the paper is on the development of the sub-reflector elements, namely the tubular hinges that use embedded heaters and sensors for actuation, the actuation mechanisms, and the lightweight sandwich construction panels. A finite element analysis parametric study assessed how design features of the hinge affect its stowage and deployment dynamics. The component fabrication and testing plans for the two-panel assembly breadboard model are outlined.
Document ID
20230013708
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Juan M Fernandez
(Langley Research Center Hampton, Virginia, United States)
Andrew F Paddock
(Langley Research Center Hampton, Virginia, United States)
Kevin S O' Neal
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Kevin Demarco
(Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
September 21, 2023
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: 41st ESA Antenna Workshop
Location: Noordwijk
Country: NL
Start Date: September 25, 2023
End Date: September 28, 2023
Sponsors: European Space Agency
Funding Number(s)
WBS: 571232.04.29.23
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
deployable reflectors
antennas
composite hinges
robotic in-space assembly
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