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The X/X/KA-band deep space transponder for the BepiColombo mission to mercury
Authors:F De Tiberis  L Simone  D Gelfusa  P Simone  R Viola  A Santoni  O Cocciolillo  M Ziarelli  F Barletta  N Salerno  M Maffei  V Nanni
Institution:1. German Aerospace Center (DLR), Berlin, Germany;2. TU Berlin, Germany;3. Moscow State University for Geodesy and Cartography (MIIGAiK), Russia;4. TU Delft, Netherlands;5. Joint institute for VLBI ERIC, Dwingeloo, Netherlands;6. Sigma Space Corporation, Lanham, MD, USA;7. NASA Goddard Space Flight Center, Greenbelt, MD, USA;8. Stinger Ghaffarian Technologies Inc., Greenbelt, MD, USA;9. Massachusetts Institute of Technology, Cambridge, MA, USA;1. Jet Propulsion Laboratory, California Institute of Technology, 4800 Oak Grove Drive, Pasadena, CA 91109-8099, United States;2. IMCCE, Observatoire de Paris, PSL Research University, CNRS, Sorbonne Université, Univ. Lille, 77 Avenue Denfert-Rochereau, 75014 Paris, France;3. NAmur Institute for CompleX SYStems, University of Namur, Rempart de la Vierge 8, B-5000 Namur, Belgium;4. Institut UTINAM, CNRS UMR 6213, Univ. Bourgogne Franche-Comté, OSU THETA, BP 1615, F-25010 Besançon Cedex, France;5. Queen Mary University of London, Mile End Rd, London, E1 4NS, United Kingdom
Abstract:This paper reports the main characteristics of the deep space transponder (DST) equipment that has been designed, developed and tested by Thales Alenia Space—Italy (TAS-I) for the European Space Agency (ESA) BepiColombo mission to Mercury.
Keywords:
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