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    BepiColombo Planetary Orbiter Payload Selection

    18 Nov 2004

    With the approval of the Solar System Working Group (SSWG), Solar System Advisory Committee (SSAC) and Science Programme Committee (SPC), the selected payload for the Mercury Planetary Orbiter now enters the final stages of the definition phase.

    On 26 February 2004, ESA issued the Mercury Planetary Orbiter (MPO) payload request for proposals. On 15 May 2004 the proposals were received and evaluated by the international Payload Review Committee (PRC), assisted by the ESTEC teams and the industrial definition study contractors.

    The PRC issued its final recommendation with a proposed payload selection and presented this to the SSWG on 12 - 13 October and to the SSAC on 19 - 20 October. Both the SSWG and SSAC have approved the proposed MPO payload selection.

    The Science Programme Committee, during its meeting on 9 - 10 November 2004, unanimously approved the proposed payload complement and this selection will now be taken by the project team for the finalisation of the definition phase and for the implementation phase.

    Selected MPO payload

    Name Payload Responsible
    BELA1 Laser Altimeter Co-PIs
    N.Thomas
    Physikalisches Institut University of Bern Switzerland
    T. Spohn
    DLR Inst. fur Planetenforschung
    Berlin
    Germany
    ISA Radio science ACC: accelerometer PI
    V. Iafolla
    CNR-IFSI
    Rome
    Itlay
    MERMAG Magnetometer PI
    A. Balogh
    The Blackett Laboratory
    Imperial College London UK
    Deputy PI
    C.M. Carr
    The Blackett Laboratory
    Imperial College London
    UK
    MERTIS-TIS IR spectrometer PI
    E.K. Jessberger
    Institut fur Planetologie
    University Munster
    Germany
    MGNS


    or


    MANGA2
    Gamma ray and neutron spectrometer PI
    I. Mitrofanov
    Institute for Space Research
    Moscow
    Russia
    PI
    C. d'Uston
    CESR
    Toulouse
    France
    Co-PIs
    N. Hasebe
    Waseda University
    Tokyo
    Japan
    G. Klingelhofer
    Johannes-Gutenberg-Univers.
    Mainz
    Germany
    MIXS X-ray spectrometer PI
    S. Dunkin
    Space Science & Technology Department
    CCLRC Rutherford Appleton Lab.
    Chilton
    UK
    Co-PI
    K. Muinonen
    Observatory Univ. of Helsinki
    Finland
    MORE Radio science
    Ka-band transponder
    PI
    L. Iess
    University of Rome "La Sapienza"
    Italy
    PHEBUS UV spectrometer PI
    E. Chassefiere
    SA/IPSL
    Universite P&M Curie Paris
    France
    Co-PIs
    S. Okano
    Planetary Plasma & Atmospheric Research Center
    Tohoku University
    Sendai
    Japan
    O. Korablev
    IKI
    Moscow
    Russia
    SERENA Neutral and ionised particle analyser PI
    S. Orsini
    CNR-IFSI
    Rome
    Italy
    Co-PIs
    S. A. Livi
    Johns Hopkins University
    Applied Physical Lab.
    Laurel
    USA
    S. Barabash
    Swedish Inst.of Space Physics (IRF)
    Kiruna
    Sweden
    K. Torkar
    Space Research Institute
    Austrian Academy of Sciences
    Graz
    Austria
    SIMBIO-SYS High resolution + stereo camerasVisual and NIR spectrometer PI
    E. Flamini
    Italian Space Agency
    Rome
    Italy
    Co-PIs
    F. Capaccioni
    INAF-IASF
    Rome
    Italy
    L. Colangeli
    INAF-Osserv.Astronomico di Capodimonte
    Napoli
    Italy
    G. Cremonese
    INAF-Osserv. Astronomico di Padova
    Italy
    A. Doressoundiram
    LESIA-Obs. de Paris
    Meudon
    France
    O. Forni
    Institut d'Astrophysique Spatiale (IAS)
    Orsay
    France
    J. L. Josset
    SPACE-X
    Space Exploration
    Neuchatel
    Switzerland
    SIXS Solar monitor PI
    J. Huovelin
    Observatory-Univ. of Helsinki
    Finland
    Co-PI
    M. Grande
    Space Science & Technol. Dept.
    CCLR-Rutherford Appleton Lab.
    Chilton
    UK

    Table Notes

    1The feasibility of the laser altimeter has to be demonstrated before November 2005, after which BELA can then be confirmed as part of the payload.

    2For the gamma-ray spectrometer there are two proposals (MGNS or MANGA). Both proposals present technical risks and the feasibility have to be demonstrated before November 2005. The MGNS, which has the lower impact on resources, is the preferred solution, and it will be confirmed as part of the payload if its feasibility is confirmed.


    Last Update: 01 Dec 2004

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