2012 IEEE International Conference on Ultra-Wideband 2012
DOI: 10.1109/icuwb.2012.6340389
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Reflectarray antennas for space applications

Abstract: In this paper, the advantages and recent developments of reflectarray antennas for space applications are reviewed. Basic requirements for space antennas, and the limitations and challenges of conventional designs are discussed. Various advantages of reflectarray antennas over reflectors and phased array antennas are reviewed and it is shown that reflectarray antennas can be a suitable low-cost choice for the new generation of space antennas.

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Cited by 9 publications
(5 citation statements)
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“…The authors in [6] extended the said path loss model to arbitrary incident angles and polarizations, but considered the far-field zone of the IRS. Recently, a stream of papers (e.g., [7], [8], and references therein) proposed a path loss model that is applicable to nearfield, using the "cos q " radiation pattern [9] for each IRS element, which differs from the plate scattering-based model.…”
Section: Introductionmentioning
confidence: 99%
“…The authors in [6] extended the said path loss model to arbitrary incident angles and polarizations, but considered the far-field zone of the IRS. Recently, a stream of papers (e.g., [7], [8], and references therein) proposed a path loss model that is applicable to nearfield, using the "cos q " radiation pattern [9] for each IRS element, which differs from the plate scattering-based model.…”
Section: Introductionmentioning
confidence: 99%
“…in which ε cd is defined as the radiation efficiency (governed by intrinsic material losses, such as dielectric and conduction losses), ε p as phase efficiency and ε b is the blockage efficiency, respectively. In this paper, we ignore the intrinsic material losses and assume a point source to illuminate the IRS aperture, the aperture efficiency of a reflecting surface is mainly dominated by spillover efficiency (ε s ) and taper efficiency (ε t ) and the rest of efficiencies are assumed to be ideal (equal to 1) [14]. Thus, the aperture efficiency can be rewritten as…”
Section: Efficiency Of Rectangular Irsmentioning
confidence: 99%
“…This is accomplished by changing the distance, R i , between the unit-cells and the feed antenna phase center. Proposed approaches include single feed systems that mechanically tune R i [48]- [51], or multiple feed systems that create discrete values of R i [52]- [54]. Multiple feed systems are not well suited for SmallSat applications since they add significant mass to the spacecraft and require individual feed networks and complicated deployment mechanisms.…”
Section: Introductionmentioning
confidence: 99%