Počet záznamů: 1
Shock deceleration in interplanetary coronal mass ejections (ICMEs) beyond Mercury's orbit until one AU
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SYSNO ASEP 0501717 Druh ASEP J - Článek v odborném periodiku Zařazení RIV J - Článek v odborném periodiku Poddruh J Článek ve WOS Název Shock deceleration in interplanetary coronal mass ejections (ICMEs) beyond Mercury's orbit until one AU Tvůrce(i) Grison, Benjamin (UFA-U) RID, ORCID
Souček, Jan (UFA-U) RID, ORCID
Krupař, Vratislav (UFA-U) RID, ORCID
Píša, David (UFA-U) RID, ORCID
Santolík, Ondřej (UFA-U) RID, ORCID
Taubenschuss, Ulrich (UFA-U) RID, ORCID
Němec, F. (CZ)Celkový počet autorů 7 Číslo článku A54 Zdroj.dok. Journal of Space Weather and Space Climate. - : EDP Sciences - ISSN 2115-7251
Roč. 8, DEC (2018)Poč.str. 10 s. Forma vydání Online - E Jazyk dok. eng - angličtina Země vyd. FR - Francie Klíč. slova interplanetary coronal mass ejection (CME) ; interplanetary medium ; propagation ; space weather ; multipoint analysis Vědní obor RIV BL - Fyzika plazmatu a výboje v plynech Obor OECD Fluids and plasma physics (including surface physics) CEP GA18-05285S GA ČR - Grantová agentura ČR GA17-08772S GA ČR - Grantová agentura ČR GJ17-06818Y GA ČR - Grantová agentura ČR Institucionální podpora UFA-U - RVO:68378289 UT WOS 000452287600002 EID SCOPUS 85058169117 DOI 10.1051/swsc/2018043 Anotace The CDPP propagation tool is used to propagate interplanetary coronal mass ejections (ICMEs) observed at Mercury by MESSENGER to various targets in the inner solar system (VEX, ACE, STEREO-A and B). The deceleration of ICME shock fronts between the orbit of Mercury and 1 AU is studied on the basis of a large dataset. We focus on the interplanetary medium far from the solor corona, to avoid the region where ICME propagation modifications in velocity and direction are the most drastic. Starting with a catalog of 61 ICMEs recorded by MESSENGER, the propagation tool predicts 36 ICME impacts with targets. ICME in situ signatures are investigated close to predicted encounter times based on velocities estimated at MESSENGER and on the default propagation tool velocity (500 km s(-1)). ICMEs are observed at the targets in 26 cases and interplanetary shocks (not followed by magnetic ejecta) in two cases. Comparing transit velocities between the Sun and MESSENGER ((v) over bar (Sunmess))and between MESSENGER and the targets ((v) over bar (MessTar)), we find an average deceleration of 170 km s(-1) (28 cases). Comparing (v) over bar (MessTar) to the velocities at the targets (v(Tar)), average ICME deceleration is about 160 km s(-1) (13 cases). Our results show that the ICME shock deceleration is significant beyond Mercury's orbit. ICME shock arrival times are predicted with an average accuracy of about six hours with a standard deviation of eleven hours. Focusing on two ICMEs detected first at MESSENGER and later on by two targets illustrates our results and the variability in ICME propagations. The shock velocity of an ICME observed at MESSENGER, then at VEX and finally at STEREO-B decreases all the way. Predicting arrivals of potentially effective ICMEs is an important space weather issue. The CDPP propagation tool, in association with in situ measurements between the Sun and the Earth, can permit to update alert status of such arrivals. 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 2019
Počet záznamů: 1