Počet záznamů: 1
Turbulence Heating ObserveR – THOR: Mission overview and payload\nsummary
- 1.
SYSNO ASEP 0459674 Druh ASEP A - Abstrakt Zařazení RIV Záznam nebyl označen do RIV Zařazení RIV Není vybrán druh dokumentu Název Turbulence Heating ObserveR – THOR: Mission overview and payload
summaryTvůrce(i) Wielders, A. (NL)
Boudin, N. (NL)
Vaivads, A. (SE)
Khotyaintsev, Y. (SE)
Lavraud, B. (FR)
Sahraoui, F. (FR)
Nakamura, R. (AT)
Owen, C. (GB)
Fazakerley, A. (GB)
Němeček, Z. (CZ)
Souček, Jan (UFA-U) RID, ORCID
Marcucci, F. (IT)
Wimmer-Schweingruber, R. (DE)
Retino, A. (FR)
Gehler, M. (NL)
Escoubet, P. (NL)Celkový počet autorů 16 Zdroj.dok. Geophysical Research Abstracts. - Göttingen : European Geosciences Union, 2016 - ISSN 1607-7962
EGU2016-15629-2Poč.str. 1 s. Forma vydání Online - E Akce EGU General Assembly 2016 Datum konání 17.04.2016-22.04.2016 Místo konání Vienna Země AT - Rakousko Typ akce WRD Jazyk dok. eng - angličtina Země vyd. DE - Německo Klíč. slova Turbulence Heating ObserveR – THOR ; plasma turbulence Vědní obor RIV BL - Fyzika plazmatu a výboje v plynech Institucionální podpora UFA-U - RVO:68378289 Anotace 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.Pracoviště Ústav fyziky atmosféry Kontakt Kateřina Adamovičová, adamovicova@ufa.cas.cz, Tel.: 272 016 012 ; Kateřina Potužníková, kaca@ufa.cas.cz, Tel.: 272 016 019 Rok sběru 2017
Počet záznamů: 1