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== Abstract ==
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In this paper a conceptual design of a SATCOM On The Move (SOTM) system in
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the Ka band is presented. This system is intended to be airborne and fully integrated in an
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AIRBUS C295 Flight Test Bench. The system relies in two separated low profile TX and RX
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antennas (about half a meter size) which reach up to 10Mbps return link and 50Mbps forward
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link.
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== Full document ==
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<pdf>Media:Draft_Content_474901375-p12-4209-document.pdf</pdf>
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== References ==
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[1] [http://Webpage:www.inmarsat.com/news/successful-airborne-testing-l-band-laisr-service Webpage:www.inmarsat.com/news/successful-airborne-testing-l-band-laisr-service]
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<span id='_GoBack'></span>[2] Webpage:northamerica.airbus-group.com/north-america/usa/Airbus-Defense-and-Space/news/press.20110221_astrium_canada
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[3] D. F. Filipovic, “A planar wideband circularly polarized antenna for satellite communications” Technologies for Wireless Applications, IEEE MTT-S Symposium on, Vancouver,BC, Canada. Feb. 1999
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[4] W.H. Weedon, S.K. Cheung, “Ku-band low-profile and wideband satellite communication antenna (LPWSA)” Phased Array Systems and Technology (PAST), Waltham, MA, USA. Oct. 2016.
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[5] G. M. Rebeiz, L. M. Paulsen, “Advances in SATCOM phased arrays using silicon technologies” Microwave Symposium, Honololu, HI, USA. Jun. 2017
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[6] [https://www.e2s2a2project.eu/ https://www.e2s2a2project.eu/]
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[7] Aeronautical Radio INCorporation, “791-1 Mark1, Aviation Ku-band and Ka band Satellite communications system” Ago. 2014
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[8] EUROCAE ED-91A “Aircraft Lightning Zoning”, Jan. 2019
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Document information

Published on 15/02/21
Accepted on 03/03/21
Submitted on 03/03/21

DOI: 10.23967/emus.2019.011
Licence: CC BY-NC-SA license

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