== Abstract ==

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In this paper a conceptual design of a SATCOM On The Move (SOTM) system in

the Ka band is presented. This system is intended to be airborne and fully integrated in an

AIRBUS C295 Flight Test Bench. The system relies in two separated low profile TX and RX

antennas (about half a meter size) which reach up to 10Mbps return link and 50Mbps forward

link.

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== Full document ==

<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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