A Foldable and Reconfigurable Monolithic Reflectarray for Space Applications
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...
Main Authors: | Abdul-Sattar Kaddour, Carlos Alberto Velez, Muhammad Hamza, Nathan C. Brown, Collin Ynchausti, Spencer P. Magleby, Larry L. Howell, Stavros V. Georgakopoulos |
---|---|
Format: | Article |
Language: | English |
Published: |
IEEE
2020-01-01
|
Series: | IEEE Access |
Subjects: | |
Online Access: | https://ieeexplore.ieee.org/document/9284423/ |
Similar Items
-
CubeSat autonomous rendezvous and docking software
by: Fear, Andrew John
Published: (2015) -
Validation of a Test Platform to Qualify Miniaturized Electric Propulsion Systems
by: Fabrizio Stesina
Published: (2019-09-01) -
Transparent Solar Panel Antenna Array
by: Yekan, Taha Shahvirdi Dizaj
Published: (2016) -
CUBESAT MISSION PLANNING TOOLBOX
by: castello, brian
Published: (2012) -
CubeSat quantum communications mission
by: Daniel KL Oi, et al.
Published: (2017-04-01)