2014
DOI: 10.1109/tap.2014.2316539
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Copper and Transparent-Conductor Reflectarray Elements on Thin-Film Solar Cell Panels

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Cited by 32 publications
(14 citation statements)
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“…There has been growing interest in combining ITO thin film technology with solar cells for satellite applications [14], [15]. However, using TCO materials in the design of the reflectarray introduces conductive losses not usually examined in reflectarray designs.…”
Section: Reflectarray Element Design Using Tcosmentioning
confidence: 99%
“…There has been growing interest in combining ITO thin film technology with solar cells for satellite applications [14], [15]. However, using TCO materials in the design of the reflectarray introduces conductive losses not usually examined in reflectarray designs.…”
Section: Reflectarray Element Design Using Tcosmentioning
confidence: 99%
“…The height of the AF32 glass is h = 1 mm, the glass is pre-cut by the manufacture to cover the solar cell seamlessly. The dielectric constant ( r ) and loss tangent (tanδ) of the AF32 glass are 4.5 and 0.015, both being measured at X band [17]. Finally, a patch antenna is screen printed on the AF32 cover glass with silver based conductive ink (124-46 by Creative Material).…”
Section: Test Fixturesmentioning
confidence: 99%
“…Such an integration can be particularly valuable for a CubeSat (a very small satellite designed with modular components to have a minimum payload) [4] as the antennas, when effectively integrated with the solar cells, do not compete with solar cells for the limited surface real estate. There have been four main types of integrations reported: (1) antennas integrated under solar cells [1,[5][6][7]; (2) antennas integrated on the same plane with or on the side wall perpendicular to solar cells [8][9][10]; (3) antennas integrated on top of solar cells [11][12][13][14][15][16][17][18], and (4) parts of the solar cells function as antenna [19][20][21] (the antenna in [7] also belongs to this category as the solar cell above the antenna acts as a parasitic elements of the antenna). The third type of integration is of particular interest and promise to a CubeSat system as the antenna topology, especially when it is small or optically transparent, facilitates a possible modular design.…”
Section: Introductionmentioning
confidence: 99%
“…In [15], optical transmittance greater than 90% was observed in graphene films with a thickness of tens of nanometres in the 400 nm -1800 nm wavelength range. Integration of optically transparent antennas with solar cell can reduce the overall system size, weight, cost and visual disturbances [16]. In space applications like satellites, size and weight of the on-board payload are the two critical parameters.…”
Section: Introductionmentioning
confidence: 99%