2017
DOI: 10.1051/e3sconf/20171603007
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Novel Concepts for High-Efficiency Lightweight Space Solar Cells

Abstract: One of the key issues in the design and development of a satellite Photovoltaic Assembly (PVA) is the trade-off to be made between the available volume located to the PVA, its mass and the total amount of power that the solar panels have to guarantee to the spacecraft. The development of high-efficiency, flexible, lightweight solar cells is therefore instrumental to the design of future satellites providing enhanced missions and services. Based on the consolidated development of GaAs-based single junction and … Show more

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Cited by 13 publications
(8 citation statements)
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“…By removing the Ge wafer, structures such as the tandem thin‐film InGaP/GaAs solar cells appear to be promising for space solar arrays. The removal of the substrate also allows access to the rear contact, resulting in the development of new architectures . Owing to the possibility of applying a back reflector, thin‐film devices require smaller active layer thicknesses, further reducing costs related to both the weight and the growth of the epitaxial layers.…”
Section: Introductionmentioning
confidence: 99%
See 1 more Smart Citation
“…By removing the Ge wafer, structures such as the tandem thin‐film InGaP/GaAs solar cells appear to be promising for space solar arrays. The removal of the substrate also allows access to the rear contact, resulting in the development of new architectures . Owing to the possibility of applying a back reflector, thin‐film devices require smaller active layer thicknesses, further reducing costs related to both the weight and the growth of the epitaxial layers.…”
Section: Introductionmentioning
confidence: 99%
“…Based on the hypothesis that the permanent displacement damage produced by the incidence of charged particles is the main aspect that degrades the device performance in space, the mission equivalent damage from electrons, protons, ions, and neutrons of different energies can be averaged by a certain electron fluence. [30][31][32][33] Geostationary orbit missions (GEO) usually last for 15 years, and the damage created by the irradiation environment is equivalent to that obtained by a fluence of 1 × 10 15 1-MeV electrons/cm 2 . For low earth orbit (LEO) missions, which last for approximate 10 years at a lower altitude, the equivalent fluences are five to 10 times lower.…”
mentioning
confidence: 99%
“…This is well known for single-junction GaAs cells and may be expected to have a similar role in QD solar cells. In [50] we have shown through physics-based simulations that under the hypothesis of very efficient photon recycling, QD-SCs might reach efficiency higher than 30%. However, from a practical standpoint, whereas in a single-junction GaAs cell a planar reflector is sufficient to achieve strong photon recycling (since photons are re-emitted isotropically), the QD cell needs at the same time texturing of the solar cell surface(s) for lighttrapping.…”
Section: Photonic Management Approaches Through Cell Nanostructuringmentioning
confidence: 99%
“…This approach enables fabrication of very thin solar cells, which would be beneficial e.g. for space and unmanned aerial vehicle applications [16,17]. As the simplest approach for improving the absorption, highly reflective planar back reflectors could effectively double the length of the optical path, increasing the J sc .…”
Section: Introductionmentioning
confidence: 99%