Segmented, Pleat-Folded and Rib-Supported Thin-Shell Composite Antenna Reflector A new architecture scalable to sizes greater than 10 m for a deployable solid surface reflector antenna is presented. The design makes use of radially and circumferentially segmented thin-shell composite gores interconnected on the back side by a series of flexible shape memory composite elements. The reflector surface stows like an umbrella by creating serpentine-shaped pleats in the thin shell while being supported by a simple-hinged metering rib structure. A parametric study assessed how design features affect the deployed stiffness of the reflector and are used to identify a test matrix for manufacturing, foldability, and shape accuracy assessments. Various manufacturing tooling designs and dedicated folding fixtures were built to increase the fidelity and confidence of the test articles produced. An overview of the development effort is provided.
Document ID
20230013559
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 P Roscoe (Langley Research Center Hampton, Virginia, United States)
Kevin Demarco (Analytical Mechanics Associates (United States) Hampton, Virginia, United States)
Date Acquired
September 19, 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, ESTEC
Funding Number(s)
WBS: 571232.04.29.23
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Deployable antennasReflectorsParametric Design Study