Published January 6, 2019 | Version public
Book Section - Chapter

Large-Area Deployable Reflectarray Antenna for CubeSats

  • 1. ROR icon Jet Propulsion Lab
  • 2. ROR icon California Institute of Technology

Abstract

Herein is described a 1.5 m x 1.5 m reflectarray antenna designed to stow in a cylinder of 20 cm diameter and 9 cm height, and then be unfolded to provide an aperture suitable for radio frequency (RF) operations at X-band (8.4 GHz) and produce 39.6 dB of gain. The mass of the reflectarray, as measured for a full-scale prototype, is 1.75 kg. The reflectarray comprises a number of crossed-dipoles held 5 mm above a ground plane. The dipole layer and the ground plane are supported by thin planar composite facesheets; the separation between these facesheets is provided by thin composite collapsible 'S'-shaped-springs. The structure is divided into a number of quartz-epoxy composite strips arranged in concentric squares and connected to each other using slipping folds. The strips can be flattened, star-folded, and wrapped to package within the compact cylindrical volume. A full-scale prototype of this reflectarray was constructed and tested. Stowage in the design volume was successfully demonstrated, and all RF performance requirements were met, as shown by a pre-stowage RF test and a post-stowage RF test.

Additional Information

© 2019 by the American Institute of Aeronautics and Astronautics, Inc. The U.S. Government has a royalty-free license to exercise all rights under the copyright claimed herein for Governmental purposes. All other rights are reserved by the copyright owner. Published Online: 6 Jan 2019.

Additional details

Identifiers

Eprint ID
99816
Resolver ID
CaltechAUTHORS:20191112-154118926

Dates

Created
2019-11-13
Created from EPrint's datestamp field
Updated
2021-11-16
Created from EPrint's last_modified field

Caltech Custom Metadata

Caltech groups
Space Solar Power Project , GALCIT
Other Numbering System Name
AIAA Paper
Other Numbering System Identifier
2019-2257