This paper describes the feasibility study of a Ka-band transceiver designed for small satellite and CubeSat operations. The transponder ensures up to 100 Mbit s1 of data rate with a target power consumption of 20W and an overall volume of 1.5U, not including the antenna. To reduce the costs, commercial off-the-shelf electronic components are used whenever possible. Exploiting a data communication interface like the one proposed, the small satellites market could be opened to new applications such as remote sensing, Earth observation and commercial telecommunications.
A Ka-band Transceiver for CubeSat Satellites: Feasibility Study and Prototype Development / Cuttin, A., Alimenti, F., Coromina, F., De Fazio, E., Dogo, F., Fragiacomo, M., Gervasoni, P., Gotti, G., Gregorio, A., Mezzanotte, P., Pagana, E., Palazzi, V., Pelusi, F., Petrini, P., Roselli, L., Vincenti Gatti, R.. - ELETTRONICO. - (2018), pp. 930-933. (48th European Microwave Conference Madrid 25/9/2018- 27/9/2018).
A Ka-band Transceiver for CubeSat Satellites: Feasibility Study and Prototype Development
P. Petrini;
2018
Abstract
This paper describes the feasibility study of a Ka-band transceiver designed for small satellite and CubeSat operations. The transponder ensures up to 100 Mbit s1 of data rate with a target power consumption of 20W and an overall volume of 1.5U, not including the antenna. To reduce the costs, commercial off-the-shelf electronic components are used whenever possible. Exploiting a data communication interface like the one proposed, the small satellites market could be opened to new applications such as remote sensing, Earth observation and commercial telecommunications.Pubblicazioni consigliate
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https://hdl.handle.net/11583/2716420
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