2008
DOI: 10.1109/maes.2008.4635069
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Ultra-lightweight space power from hybrid thin-film solar cells

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Cited by 11 publications
(8 citation statements)
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References 47 publications
(38 reference statements)
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“…[ 4,5 ] However, the output power (1–2 W) generated by a single SC is not enough for space vehicles that require several kW of electric power, thus solar arrays are used. [ 6,7 ] A solar array is made up by several solar panels (or modules), that comprise more SCs connected together (in series and/or parallel ways). Quite differently, for satellites for outer planets missions (i.e., Jupiter 5.2 AU, Saturn 9.6 AU, Uranus 19.2 AU, and Neptune 30.0 AU) [ 3 ] working in low intensity low temperature conditions, NPSs seem the best solution to satisfy mission requirements.…”
Section: Introductionmentioning
confidence: 99%
“…[ 4,5 ] However, the output power (1–2 W) generated by a single SC is not enough for space vehicles that require several kW of electric power, thus solar arrays are used. [ 6,7 ] A solar array is made up by several solar panels (or modules), that comprise more SCs connected together (in series and/or parallel ways). Quite differently, for satellites for outer planets missions (i.e., Jupiter 5.2 AU, Saturn 9.6 AU, Uranus 19.2 AU, and Neptune 30.0 AU) [ 3 ] working in low intensity low temperature conditions, NPSs seem the best solution to satisfy mission requirements.…”
Section: Introductionmentioning
confidence: 99%
“…In fact, the possibility to build transparent or semitransparent photovoltaic panels makes DSCs suitable not only for roof mounting, but also for integration in windows, shelters, and facade decorations. In addition, they are very promising for all those applications where costs and power-to-weight ratio have to reach the best trade-off [5]. Incidentally, the development of hybrid solar cells on flexible, lightweight, and durable substrates provides an attractive solution for energy conversion with high mass specific power (W/Kg).…”
Section: Introductionmentioning
confidence: 99%
“…In particular, modern spacecraft need several kilowatts of electric energy, 3 , 4 which is usually produced through photovoltaic (PV) technologies because of the abundance of solar energy and safety requirements, making them preferable to alternatives such as batteries, fuel cells, and nuclear power. 5 , 6 For example, the International Space Station contains four solar arrays made up by >260 000 Si-based solar cells (SCs) producing up to 120 kW.…”
mentioning
confidence: 99%
“…In particular, modern spacecraft need several kilowatts of electric energy, , which is usually produced through photovoltaic (PV) technologies because of the abundance of solar energy and safety requirements, making them preferable to alternatives such as batteries, fuel cells, and nuclear power. , For example, the International Space Station contains four solar arrays made up by >260 000 Si-based solar cells (SCs) producing up to 120 kW . However, finding materials suitable for space applications is not a trivial task because there are several requirements that must be met: (i) resistance to the harsh space environment, (ii) low weight, (iii) high power conversion efficiency (PCE), and (iv) high gravimetric power (W kg –1 ). ,, Moreover, the cost of PV technologies represents another important factor especially for the realization of extra-terrestrial habitable stations (for example, on the Moon and Mars) and for the new opportunities opened up by the privatization of the space industry (such as space tourism) .…”
mentioning
confidence: 99%
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