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  • Keynote: copernicus sentinel-1: satellite outline and early results

    Paper number

    IAC-14,B1,1,1,x26214

    Author

    Mr. Aniceto Panetti, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Friedhelm Rostan, Airbus Defence and Space, Germany

    Coauthor

    Dr. Michelangelo L'Abbate, Thales Alenia Space Italia, Italy

    Coauthor

    Dr. Claudio Bruno, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Roberto Baldassarri, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Antonio Bauleo, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Toni Catalano, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Marco Enrico Maria Cotogni, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Luigi Galvagni, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Fabio Ippoliti, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Pierluigi Petrini, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Sergio Pica, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Andrea Pietropaolo, Thales Alenia Space Italia, Italy

    Coauthor

    Ms. Francesca Spataro, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Giacomo Taini, Thales Alenia Space Italia, Italy

    Coauthor

    Dr. Paolo Venditti, Thales Alenia Space Italia, Italy

    Coauthor

    Mr. Mathias von Alberti, Airbus Defence and Space, Germany

    Coauthor

    Dr. Ramon Torres, European Space Agency (ESA), The Netherlands

    Coauthor

    Mr. Svein Lokas, European Space Agency (ESA), The Netherlands

    Coauthor

    Mr. David Bibby, ESA, The Netherlands

    Year

    2014

    Abstract
    The GMES Sentinel-1 Earth Radar Observatory, a project funded by the European Union and developed by ESA, is a constellation of two C-band radar satellites. The satellites have been conceived to be a continuous and reliable source of C-band SAR imagery for operational application such as mapping of global landmasses, coastal zones and monitoring of shipping routes. The Sentinel-1 satellites are built by an industrial consortium headed by Thales Alenia Space Italy as Prime Contractor. The paper presents an outline of the general satellite architecture, the spacecraft subsystems, AIT flow and satellite key performances. The GMES Sentinel-1 satellite represents the state of the art for a LEO spacecraft, in terms of SAR performances, avionics performances, data storage and transmission capability, optical communication link capability, electrical power generation and management and large payload accommodation capability of PRIMA bus.
    The key payload is the C-SAR instrument, which has been developed and built under the responsibility of AIRBUS Defence & Space. The C-SAR Instrument has to provide a dual polarisation capability as well as four operational modes, i.e. Stripmap, Interferometric wideswath, Extra Wideswath as well as Wave Mode. These shall allow for resolutions of up to 5 m x 5 m as well as for swath widths up to 400 km. The demanding operational requirements require an active phased array antenna allowing a fast beam shaping and steering capability in both azimuth an elevation as well as a powerful central electronics for command and control of the whole SAR instrument including pulse generation and echo reception, down-conversion, compression and formatting.
    
    Sentinel-1 spacecraft has just successfully completed its full space qualification program and has now been shipped to the Guyana Space Centre for a Soyuz launch. The paper will present the final results of Sentinel-1 on ground qualification and test programme and the early results of in orbit commissioning.
    Abstract document

    IAC-14,B1,1,1,x26214.brief.pdf

    Manuscript document

    IAC-14,B1,1,1,x26214.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.