Shock deceleration in interplanetary coronal mass ejections (ICMEs) beyond Mercury's orbit until one AU

Kód výsledku v IS VaVaI

<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F00216208%3A11320%2F18%3A10391205" target="_blank" >RIV/00216208:11320/18:10391205 - isvavai.cz</a>

Nalezeny alternativní kódy

RIV/68378289:_____/18:00501717

Výsledek na webu

<a href="https://doi.org/10.1051/swsc/2018043" target="_blank" >https://doi.org/10.1051/swsc/2018043</a>

DOI - Digital Object Identifier

<a href="http://dx.doi.org/10.1051/swsc/2018043" target="_blank" >10.1051/swsc/2018043</a>

Jazyk výsledku

angličtina

Název v původním jazyce

Shock deceleration in interplanetary coronal mass ejections (ICMEs) beyond Mercury's orbit until one AU

Popis výsledku v původním jazyce

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&apos;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.

Název v anglickém jazyce

Shock deceleration in interplanetary coronal mass ejections (ICMEs) beyond Mercury's orbit until one AU

Popis výsledku anglicky

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&apos;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.

Druh

J_imp - Článek v periodiku v databázi Web of Science

CEP obor

—

OECD FORD obor

10305 - Fluids and plasma physics (including surface physics)

Projekt

Výsledek vznikl pri realizaci vícero projektů. Více informací v záložce Projekty.

Návaznosti

I - Institucionalni podpora na dlouhodoby koncepcni rozvoj vyzkumne organizace

Rok uplatnění

2018

Kód důvěrnosti údajů

S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Název periodika

Journal of Space Weather and Space Climate

ISSN

2115-7251

e-ISSN

—

Svazek periodika

8

Číslo periodika v rámci svazku

Dec

Stát vydavatele periodika

FR - Francouzská republika

Počet stran výsledku

10

Strana od-do

—

Kód UT WoS článku

000452287600002

EID výsledku v databázi Scopus

2-s2.0-85058169117