Flexible High-Efficiency Corrugated Monocrystalline Silicon Solar Cells for Application in Small Unmanned Aerial Vehicles for Payload Transportation
dc.contributor.author | Elatab, Nazek | |
dc.contributor.author | Khan, Sherjeel M. | |
dc.contributor.author | Hussain, Muhammad Mustafa | |
dc.date.accessioned | 2020-08-13T13:40:50Z | |
dc.date.available | 2020-08-13T13:40:50Z | |
dc.date.issued | 2020-08-17 | |
dc.date.submitted | 2020-07-21 | |
dc.identifier.citation | El-Atab, N., Khan, S. M., & Hussain, M. M. (2020). Flexible High-Efficiency Corrugated Monocrystalline Silicon Solar Cells for Application in Small Unmanned Aerial Vehicles for Payload Transportation. Energy Technology. doi:10.1002/ente.202000670 | |
dc.identifier.issn | 2194-4288 | |
dc.identifier.issn | 2194-4296 | |
dc.identifier.doi | 10.1002/ente.202000670 | |
dc.identifier.doi | 10.1002/ente.202070111 | |
dc.identifier.uri | http://hdl.handle.net/10754/664582 | |
dc.description.abstract | In recent years, small unmanned aerial vehicles (SUAVs) have proven to be exceptionally useful. However, most of the commercially available drones are electric powered and therefore have a short endurance. Solar powered UAVs have recently received increased attention due to their ability to fly continuously for several days using solar energy. For this purpose, solar cells must show high-efficiency, lightweight and ultra-flexibility in order to be fully compliant to the drone wings/body and avoid degrading its aerodynamic characteristics. Nevertheless, previous demonstrations used rigid/semi-flexible cells. Here, corrugated ultra-flexible silicon solar cells (19% efficiency) with a smaller specific weight (645 g/m2, encapsulated) are considered and used. A theoretical comparison between the performances of the corrugated vs. commercial semi-flexible cells is performed in terms of flight endurance in “AtlantikSolar” UAV. The results show that due to the ultra-lightweight of the corrugated cells and their ability to expand at higher temperatures without bowing, an enhancement in the flight time up to 19% can be achieved compared to the commercial cells which enables heavier payloads (7 lbs) transportation. Finally, the corrugated cells (12.5 cm by 4 cm) are experimentally tested on a small-sized drone under different conditions indoors and a 10% extended flight is reported. | |
dc.description.sponsorship | The work is supported by the Lockheed Martin and King Abdullah University of Science and Technology (KAUST) Office of Sponsored Research (OSR). | |
dc.publisher | Wiley | |
dc.relation.url | https://onlinelibrary.wiley.com/doi/abs/10.1002/ente.202000670 | |
dc.rights | Archived with thanks to Energy Technology | |
dc.title | Flexible High-Efficiency Corrugated Monocrystalline Silicon Solar Cells for Application in Small Unmanned Aerial Vehicles for Payload Transportation | |
dc.type | Article | |
dc.contributor.department | Computer, Electrical and Mathematical Sciences and Engineering (CEMSE) Division | |
dc.contributor.department | Electrical Engineering Program | |
dc.contributor.department | Integrated Nanotechnology Lab | |
dc.identifier.journal | Energy Technology | |
dc.rights.embargodate | 2022-07-21 | |
dc.eprint.version | Post-print | |
dc.contributor.institution | EECSUniversity of California Berkeley CA 94720 USA | |
kaust.person | Elatab, Nazek | |
kaust.person | Khan, Sherjeel | |
kaust.person | Hussain, Muhammad Mustafa | |
dc.date.accepted | 2020-08-04 | |
refterms.dateFOA | 2020-08-13T13:44:26Z | |
kaust.acknowledged.supportUnit | Office of Sponsored Research (OSR) | |
dc.date.published-online | 2020-08-17 | |
dc.date.published-print | 2020-11 |
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