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Turbulence Heating ObserveR – THOR: Mission overview and payload\nsummary

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    0459674 - ÚFA 2017 DE eng A - Abstract
    Wielders, A. - Boudin, N. - Vaivads, A. - Khotyaintsev, Y. - Lavraud, B. - Sahraoui, F. - Nakamura, R. - Owen, C. - Fazakerley, A. - Němeček, Z. - Souček, Jan - Marcucci, F. - Wimmer-Schweingruber, R. - Retino, A. - Gehler, M. - Escoubet, P.
    Turbulence Heating ObserveR – THOR: Mission overview and payload
    summary.
    Geophysical Research Abstracts. Göttingen: European Geosciences Union, 2016. EGU2016-15629-2. ISSN 1607-7962.
    [EGU General Assembly 2016. 17.04.2016-22.04.2016, Vienna]
    Institutional support: RVO:68378289
    Keywords : Turbulence Heating ObserveR – THOR * plasma turbulence
    Subject RIV: BL - Plasma and Gas Discharge Physics
    http://meetingorganizer.copernicus.org/EGU2016/EGU2016-15629-2.pdf

    The Turbulence Heating ObserveR (THOR) mission was selected as one of the three candidates of the Call for
    Medium Class Missions M4 in the European Space Agency’s Science Programme with a launch planned in 2026.
    THOR is the first mission ever flown in space dedicated to plasma turbulence. THOR will lead to an understanding
    of the basic plasma heating and particle energization processes, of their effect on different plasma species and of
    their relative importance in different turbulent regimes. The THOR mission features one single spinning spacecraft
    with 10 scientific instruments focusing on particular regions in three different elliptical orbits around the Earth;
    pristine solar wind, Earth’s bow shock and interplanetary shocks, and compressed solar wind regions downstream
    of shocks.
    These regions are selected because of their differing turbulent fluctuation characteristics, and reflect similar astrophysical
    environments. The THOR mission, the conceptual design of the spacecraft and a summary of the payload
    will be presented. Furthermore, driving requirements and their implications for the spacecraft like Electromagnetic
    Compatibility and cleanliness will be discussed.
    Permanent Link: http://hdl.handle.net/11104/0259853

     
     
Number of the records: 1  

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