A Foldable and Reconfigurable Monolithic Reflectarray for Space Applications
Abdul-Sattar Kaddour, Carlos A. Velez, Muhammad Hamza, Nathan Brown, Collin Ynchausti, Spencer P. Magleby, Larry L. Howell, Stavros V. Georgakopoulos
Abstract
An origami-based foldable and reconfigurable Reflectarray Antenna (RA) with multiple apertures is proposed for CubeSat applications. The proposed configuration consists of a central RA embedded in folding panels using Lamina Emergent Torsional (LET) joints based on compliant mechanisms. Depending on the folding direction of these panels (forward or backward), a new RA aperture is formed. The proposed RA along with its folding panels and hinges is fabricated using only a single PCB. A prototype of such an RA with two foldable panels is fabricated and measured. This RA operates in the Ku-band at 16 GHz and provides two pencil beams pointing at (8 = 30°, φ = 0°) and (8 = -30°, φ = 0°), and a dual-beam pointing at (8 = +27°, φ = 0°) and (8 = -29°, φ = 0°). The proposed RA provides a gain of 25 dB and 19 dB in its singleand dual-beam operations, respectively. For CubeSat applications, the key advantages of this RA are its small stowed volume, reconfigurable EM performance, beamsteering capabilities, monolithic construction, low fabrication cost, and reduced complexity.