2020 IEEE International Conference on Wireless for Space and Extreme Environments (WiSEE) 2020
DOI: 10.1109/wisee44079.2020.9262670
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Thickness-Accommodation in X-Band Origami-based Reflectarray Antenna for Small Satellites Applications

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Cited by 15 publications
(5 citation statements)
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“…This concept of using unique features on each unit is prohibitively costly when using traditional photographically, but easy to integrate on an AM production process with no added cost. The manufacturing process of RF front-end devices has been benefiting from additive manufacturing (AM) techniques and their capabilities, such as rapid prototyping and conformal designs, that traditional manufacturing cannot achieve [27]. The underlying concept of AMEF is to intentionally modify the fingerprint of RF transceivers and leverage its uniqueness to enhance the security of wireless systems.…”
Section: Osi Layermentioning
confidence: 99%
“…This concept of using unique features on each unit is prohibitively costly when using traditional photographically, but easy to integrate on an AM production process with no added cost. The manufacturing process of RF front-end devices has been benefiting from additive manufacturing (AM) techniques and their capabilities, such as rapid prototyping and conformal designs, that traditional manufacturing cannot achieve [27]. The underlying concept of AMEF is to intentionally modify the fingerprint of RF transceivers and leverage its uniqueness to enhance the security of wireless systems.…”
Section: Osi Layermentioning
confidence: 99%
“…The literature reveals incremental advancements in reflectarray technology, including efforts to utilize inkjet printing for antenna fabrication, explore flexible substrates for enhanced mechanical versatility, and apply origami principles for deployable structures [1][2][3][4][5][6][7]. However, existing studies typically address these aspects in isolation, focusing on either the manufacturing technique, the substrate material, or the deployment mechanism without fully integrating these components into a singular, cohesive design.…”
Section: Introductionmentioning
confidence: 99%
“…However, these designs focus on small aperture FPRs stowed on the exterior of the CubeSat buses. In [24], a large aperture (64.2 cm × 64.2 cm) origami-based deployable FPR was presented. However, the stowed dimensions of the FPR (13.5 cm × 10.0 cm × 6.2 cm) prevent it from being stowed within the volume of a standard CubeSat unit (1U = 10 cm × 10 cm × 10 cm).…”
Section: Introductionmentioning
confidence: 99%