ORIGINAL RESEARCH article

Front. Astron. Space Sci., 21 October 2022

Sec. Space Physics

Volume 9 - 2022 | https://doi.org/10.3389/fspas.2022.952486

Dependence of radiation belt flux depletions at geostationary orbit on different solar drivers during intense geomagnetic storms

  • 1. State Key Laboratory of Marine Geology, School of Ocean and Earth Science, Tongji University, Shanghai, China

  • 2. Space Physics Laboratory, Vikram Sarabhai Space Centre, Thiruvananthapuram, India

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Abstract

The loss of electron flux of the outer radiation belt has been widely studied in terms of the mechanism that brings in these losses. There are a few studies which have attempted to explain the interplanetary conditions that favor the depletions. As the Sun is the prime cause of any change happening in the magnetosphere, it is important to look at the solar drivers that bring in such changes. In this study, we attempt to understand the effect of solar structures and substructures on the loss of radiation belt high-energy electrons during intense geomagnetic storms. The superposed epoch analysis is used to observe any peculiar changes in GOES electron flux data during the storms that are associated with solar structures such as CME and CIR, ICME substructures such as the magnetic cloud, magnetic cloud with sheath, ejecta, ejecta with sheath, and only sheath. The long-term data also give an opportunity to compare the flux decrease during solar cycles 23 and 24. It has been observed that 1) CIR-associated storms cause a comparatively higher flux decrease than CME-associated storms, 2) sheath-related storms bring out a higher flux decrease, and 3) there is no significant change in flux for the storms of both the solar cycles. The flux decrease in intense storms at the geostationary orbit is essentially triggered by the “Dst effect.” Apart from this, the minimum IMF Bz and northward IMF Bz before turning southward add to the flux decrease. These results hold true for the electron depletions occurring only during intense geomagnetic storms and may alter otherwise.

Introduction

The outer radiation belts are very much vibrant in the sense that they undergo many dynamic processes such as particle acceleration (Summers et al., 1998; Friedel et al., 2002; Elkington et al., 2003; Meredith et al., 2003; Horne et al., 2005; Reeves et al., 2013), transport (Lyons & Thorne, 1973; Baker et al., 2007), and loss (Iles et al., 2002; Onsager et al., 2002; Reeves et al., 2003; Bortnik et al., 2006; Millan & Thorne, 2007; Baker et al., 2016). Among these processes, the true loss of radiation belt particles is of prime concern because they can cause significant spacecraft operational anomalies (Baker et al., 1987; Allen, 2002; Baker et al., 2004), sometimes causing permanent damage to space systems (Baker et al., 2018) and posing a threat to the climate through instances of highly energetic electron precipitation into the atmosphere (Clilverd et al., 2016; Tsurutani et al., 2016; Baker et al., 2018). These reasons make it necessary to thoroughly study the outer belt particle losses, especially of the highly energetic electrons.

Many researchers have given special attention to understand the mechanism behind the true loss of these electrons. The observed loss of electron flux is attributed to adiabatic losses (McIlwain, 1966; Kim and Chan, 1997) or real losses either by magnetopause shadowing (Shprits et al., 2006; Baker et al., 2016; Herrera et al., 2016; Zhang et al., 2016) or precipitation into the atmosphere (Thorne & Kennel, 1971; Green et al., 2004; Turner et al., 2014; Shprits et al., 2016; Tsurutani et al., 2016; Pham et al., 2017) by resonant wave–particle interaction. Li et al. (1997) used multi-satellite observations during geomagnetic storms to suggest adiabatic losses in the inner part of the belt, whereas nonadiabatic losses in the outer part. Later, Onsager et al. (2002) also came to a similar conclusion by using multi-spacecraft observations. Bortnik et al. (2006) suggested that at high L-shells (L > 5), the dropout is independent of energy and caused due to magnetopause shadowing in addition to radial diffusion, whereas at L < 5, the dropout is strongly energy dependent and caused due to electromagnetic ion cyclotron (EMIC)–driven pitch angle scattering. Contradicting results have been obtained by Xiang et al. (2017), suggesting the importance of µ and K dependence of electron phase space density (PSD) in understanding the dropout mechanism.

Very few studies have focused on the influence of different interplanetary parameters on the loss of radiation belt electrons. Borovsky and Denton (2010) studied the solar wind effect on electron flux dropouts during geomagnetic storms, using superposed epoch analysis. Similar studies have been undertaken by Meredith et al. (2011) for high-speed solar wind (HSS)–driven storms and by Yuan and Zong (2013). They concluded that the southward interplanetary magnetic field (IMF) and high pressure led to the strongest dropouts. Gao et al. (2015) also came to a similar conclusion by studying the dropouts occurring during both storm and non-storm periods for >2 MeV electrons. Boynton et al. (2016, 2017) carried out an error reduction ratio analysis to explore the nonlinear relationship between electron dropouts and solar wind, as well as other geomagnetic indices. Ni et al. (2016) from their study of the dynamic response of the Earth’s radiation belts during periods of solar wind dynamic pressure pulse based on normalized superposed epoch analysis suggested that deeper earthward magnetopause erosion provides favorable conditions for the prompt occurrence of dropout at lower L-shells (L < 5). Pinto et al. (2018) by using GOES 8 and 10 electron flux data of energy >2 Mev studied the role of interplanetary parameters on the relativistic flux enhancements and persistent depletion events. These studies have established the role of solar wind conditions in favoring the radiation belt electron losses. From their study on the interplanetary shock properties and preconditions, Yue and Zong (2011) concluded that the perpendicular shock can produce more intense geomagnetic disturbance under the same IMF precondition. They also suggested that the interplanetary shocks can intensify the southward IMF precondition by a factor of 3–6. This study suggests that the orientation of the shocks and preconditioning are also important while considering their impact on the magnetosphere. As the Sun is the ultimate source of any change seen in the interplanetary medium, it thereby causes the magnetosphere to alter. This fact highlights the importance of studying the effect of various solar drivers on the radiation belt electron flux decrease. There are very few studies which have attempted to understand the effect of different solar structures on the radiation belt electron fluxes. Benacquista et al. (2018) studied the impact of two different solar structures, that is, the corotating interaction region (CIR) and interplanetary coronal mass ejection (ICME), on the variations of radiation belt electron fluxes. Their study revealed that the ICMEs are effective at all L-shells, whereas the CIRs have much less access to the innermost parts of the belts. Recently, Turner et al. (2019) showed that storms driven by coronal mass ejection (CME) sheaths or CME ejecta only are capable of producing prolonged depletions of multi-MeV electrons throughout the outer belt. By contrast, storms driven by full CMEs and stream interaction regions are prone to enhance MeV electrons. All these studies suggest the complexity and diversity of the radiation belt response to a space weather event at a given point of time. There has been ample research on the loss mechanism of the outer belt energetic electrons and also on the solar wind conditions which favor these losses. But, there are very few studies which have established a link between the solar structures and outer radiation belt response. Different heliospheric structures interact with the magnetosphere differently through variable forcing (Kilpua et al., 2009). All these in turn affect the response of the radiation belt electron flux. Not only the conditions within these structures are important but also in a broader way, the impacts these structures have can be different. There are still few open questions that need to be answered: 1) how differently do solar structures affect the energetic electron population of the outer radiation belt? 2) Why do two similar solar structures have different impacts on the magnetosphere? 3) Can we anticipate the response of the radiation belt if we know a particular solar structure is heading towards the Earth? 4) Is there any variation in the radiation belt flux from one solar cycle to another? In the present study, we try to investigate the response of the energetic electrons in terms of flux depletion to different solar structures. The long-term data set also provides an opportunity to compare this response over two solar cycles. We identified the flux depletions of electrons having energies >0.6 MeV and >0.8 MeV at the geostationary orbit during 103 intense geomagnetic storms that occurred between 1996 and 2019, which comprises solar cycles 23 and 24. We performed the epoch analysis to understand the contribution of different solar wind and interplanetary conditions. We have divided the events as per the solar structure which drives the changes in the magnetosphere. Firstly, the solar structures are characterized as CME or CIR. When it is CME, then depending on the ICME structure, they are further divided into magnetic cloud (MC), ejecta (EJ), sheath (S), magnetic cloud with sheath (MC-S), and ejecta with sheath (EJ-S).

Materials and methods

The intense geomagnetic storms (Dst ≤ −100 nT) that have occurred during solar cycles 23 and 24 were identified from the World Data Center (http://wdc.kugi.kyoto-u.ac.jp/dst_final/index.html). A total of 103 intense geomagnetic storms had been identified from 1996 to 2019. In order to check the electron depletions during all the selected events, the electron flux data of energy >0.6 MeV was obtained from the Geostationary Operational Environmental Satellite (GOES) 8 and 10 till 2006. From 2011 onward, we have made use of >0.8 MeV channel from GOES 15 spacecraft. The list of the energy channels and spacecraft used is given in Table 1. These data can be found at https://www.ngdc.noaa.gov/stp/satellite/goes/dataaccess.html. We made use of the OMNIWeb data (https://omniweb.gsfc.nasa.gov/form/dx1.html) to identify solar structures and substructures. The same set of data was used to examine the interplanetary conditions during the flux depletion events. Figure 1 shows the number of geomagnetic storms that occurred during solar cycles 23 and 24, which are further divided into solar structures such as CME and CIR. A total of 81 intense geomagnetic storms occurred during solar cycle 23, out of which 73 were associated with CME and 8 were associated with CIR. As we all know, solar cycle 24 was mild. It consisted of only 22 intense geomagnetic storms, out of which 21 were associated with CME and only 1 was associated with CIR. The CMEs were further divided into ICME substructures such as MC, MC-S, EJ, EJ-S, and S.

TABLE 1

Sr. No.DateSpacecraftEnergy channelType of solar structure
123 October 1996GOES 8>0.6 MeVCIR
221 April 1997GOES 8>0.6 MeVMC
315 May 1997GOES 8>0.6 MeVMC
411 October 1997GOES 8>0.6 MeVMC
507 November 1997GOES 8>0.6 MeVEJ-S
623 November 1997GOES 8>0.6 MeVMC
718 February 1998GOES 8>0.6 MeVMC
810 March 1998GOES 8>0.6 MeVCIR
904 May 1998GOES 8>0.6 MeVS
1026 June 1998GOES 8>0.6 MeVEJ
1106 August 1998GOES 8>0.6 MeVEJ
1227 August 1998GOES 8>0.6 MeVEJ
1325 September 1998GOES 8>0.6 MeVEJ
1419 October 1998GOES 8>0.6 MeVMC
1508 November 1998GOES 8>0.6 MeVEJ
1609 November 1998GOES 8>0.6 MeVS
1713 November 1998GOES 8>0.6 MeVMC
1813 January 1999GOES 8>0.6 MeVMC
1918 February 1999GOES 8>0.6 MeVEJ
2022 September 1999GOES 8>0.6 MeVEJ
2122 October 1999GOES 8>0.6 MeVEJ-S
2213 November 1999GOES 8>0.6 MeVMC
2312 February 2000GOES 8>0.6 MeVS
2407 April 2000GOES 8>0.6 MeVEJ-S
2524 May 2000GOES 8>0.6 MeVEJ
2616 July 2000GOES 8>0.6 MeVMC-S
2711 August 2000GOES 8>0.6 MeVEJ
2812 August 2000GOES 8>0.6 MeVMC
2917 September 2000GOES 8>0.6 MeVMC-S
3005 October 2000GOES 8>0.6 MeVEJ
3114 October 2000GOES 8>0.6 MeVMC
3229 October 2000GOES 8>0.6 MeVMC
3306 November 2000GOES 8>0.6 MeVMC
3429 November 2000GOES 8>0.6 MeVEJ
3520 March 2001GOES 8>0.6 MeVMC
3631 March 2001GOES 8>0.6 MeVMC-S
3711 April 2001GOES 8>0.6 MeVEJ
3818 April 2001GOES 8>0.6 MeVMC
3922 April 2001GOES 8>0.6 MeVMC-S
4017 August 2001GOES 8>0.6 MeVEJ
4126 September 2001GOES 8>0.6 MeVEJ
4201 October 2001GOES 8>0.6 MeVMC
4303 October 2001GOES 8>0.6 MeVMC
4421 October 2001GOES 8>0.6 MeVEJ
4528 October 2001GOES 8>0.6 MeVEJ
4606 November 2001GOES 8>0.6 MeVEJ
4724 November 2001GOES 8>0.6 MeVMC-S
4824 March 2002GOES 8>0.6 MeVMC
4920 April 2002GOES 8>0.6 MeVMC
5011 May 2002GOES 8>0.6 MeVEJ
5123 May 2002GOES 8>0.6 MeVMC
5202 August 2002GOES 8>0.6 MeVMC
5321 August 2002GOES 8>0.6 MeVEJ
5404 September 2002GOES 8>0.6 MeVCIR
5508 September 2002GOES 8>0.6 MeVEJ
5601 October 2002GOES 8>0.6 MeVMC
5704 October 2002GOES 8>0.6 MeVEJ
5807 October 2002GOES 8>0.6 MeVCIR
5914 October 2002GOES 8>0.6 MeVCIR
6021 November 2002GOES 8>0.6 MeVCIR
6130 May 2003GOES 8>0.6 MeVEJ
6218 June 2003GOES 10>0.6 MeVS
6312 July 2003GOES 10>0.6 MeVCIR
6418 August 2003GOES 10>0.6 MeVMC
6530 October 2003GOES 10>0.6 MeVMC
6630 October 2003GOES 10>0.6 MeVMC
6720 November 2003GOES 10>0.6 MeVMC
6822 January 2004GOES 10>0.6 MeVEJ
6904 April 2004GOES 10>0.6 MeVMC
7025 July 2004GOES 10>0.6 MeVMC
7127 July 2004GOES 10>0.6 MeVEJ
7230 August 2004GOES 10>0.6 MeVMC
7308 November 2004GOES 10>0.6 MeVMC
7418 January 2005GOES 10>0.6 MeVEJ
7515 May 2005GOES 10>0.6 MeVMC
7630 May 2005GOES 10>0.6 MeVEJ
7713 June 2005GOES 10>0.6 MeVMC
7824 August 2005GOES 10>0.6 MeVS
7931 August 2005GOES 10>0.6 MeVCIR
8011 September 2005GOES 10>0.6 MeVEJ
8115 December 2006GOES 10>0.6 MeVMC
8206 August 2011GOES 15>0.8 MeVEJ
8326 September 2011GOES 15>0.8 MeVEJ-S
8425 October 2011GOES 15>0.8 MeVMC
8509 March 2012GOES 15>0.8 MeVMC
8624 April 2012GOES 15>0.8 MeVMC
8715 July 2012GOES 15>0.8 MeVEJ
8801 October 2012GOES 15>0.8 MeVMC-S
8909 October 2012GOES 15>0.8 MeVMC
9014 November 2012GOES 15>0.8 MeVMC
9117 March 2013GOES 15>0.8 MeVMC-S
9201 June 2013GOES 15>0.8 MeVMC-S
9329 June 2013GOES 15>0.8 MeVS
9419 February 2014GOES 15>0.8 MeVEJ-S
9517 March 2015GOES 15>0.8 MeVMC-S
9623 June 2015GOES 15>0.8 MeVMC
9707 October 2015GOES 15>0.8 MeVCIR
9820 December 2015GOES 15>0.8 MeVMC
9901 January 2016GOES 15>0.8 MeVMC
10013 October 2016GOES 15>0.8 MeVMC
10128 May 2017GOES 15>0.8 MeVMC
10208 September 2017GOES 15>0.8 MeVMC
10326 August 2018GOES 15>0.8 MeVMC

List of events considered in this study along with the GOES spacecraft, the energy channel used, and the type of solar structure associated.

FIGURE 1

The identification of CMEs that occurred in solar cycle 23 was done using the catalog by Gopalswamy et al. (2010) along with the list provided by Richardson and Cane (2010). The identification of CMEs that occurred in solar cycle 24 was done by running movies of coronagraph images available at https://cdaweb.gsfc.nasa.gov. Few of the CMEs were identified using the list provided by Richardson and Cane (2010). The storms which were not associated with CME were checked for any CIR association. Such storms were identified using WIND and ACE observations. Furthermore, the substructures of CMEs were identified by their signatures in interplanetary data. The magnetic clouds (MC) were thought to have one or more of the following signatures: 1) strong magnetic field, 2) smooth latitudinal rotation of the field, and 3) low proton temperature or plasma β (Selvakumaran et al., 2016). Whereas, ejecta (EJ) had 1) a comparatively weaker magnetic field, 2) higher proton temperature or higher plasma β, 3) no clear rotation in the magnetic field, and 4) an enhanced Nα/Np ratio (Gopalswamy et al., 2010). During sheaths, no particular change was observed in plasma β, and there was no smooth rotation of the magnetic field. Major events were taken from the MC list provided by Gopalswamy et al. (2015). Other events were identified by ourselves. The respective number of storms in each category is presented in Figure 1. The storms that occurred due to MC are dominant in both solar cycles, making 45 out of a total of 103 storms, followed by 29, 9, 6, and 5 storms associated with EJ, MC-S, S, and EJ-S, respectively.

Epoch analysis was carried out to understand the effect of different solar drivers on the relativistic electron flux decrease at a geostationary orbit. The time of minimum Dst was taken as the epoch. The flux decrease (∆F) was calculated by subtracting the minimum flux from the pre-depletion value. To do this, the flux was normalized by the pre-depleted flux value. For easy understanding, we present these values in terms of the order of magnitude. We took care of the flux depletions that occurred on the same day but not during the storm period, that is, we strictly chose the depletions that occurred during the main phase of the geomagnetic storm.

Observations and results

A total of 103 intense geomagnetic storms were considered in this study that had occurred from 1996 to 2019, comprising two solar cycles. The reason behind choosing only intense storms is that not all storms produce electron flux depletions (Reeves et al., 2003). The main motive of this study was to check the dependence of electron flux decrease on different solar drivers. We calculated the level of flux decrease for each of the storms after performing superposed epoch analysis and tried to find any relationship that it may have with different solar drivers.

Epoch analysis

With the time of minimum Dst as an epoch, the epoch analysis was performed on various interplanetary conditions for different solar drivers. The magnetopause standoff distance was also considered in the analysis, which was calculated by using the model given by Shue et al. (1997). We chose a time window of 1 day before and after the epoch to examine full depletion till its recovery. Figure 2 represents the mean value of A) IMF Bz (nT); B) solar wind speed, Vsw (km/h); C) solar wind density, Np (n/cc); D) solar wind dynamic pressure, Pdy (nPa); E) electric field (V/m); F) Sym-H (nT); G) magnetopause stand-off distance, R0 (RE); and H) GOES >0.6 MeV electron flux (e cm−2 s−1 sr−1) for the different abovementioned ICME structures, shown using different colors. From the figure, it can be seen that the level of electron flux decrease is independent of the Sym-H values. This analysis reveals that the storms which are associated with sheath (MC-S, EJ-S, and S) show more flux decrease (∆F) than non-sheath drivers (MC and EJ). The highest flux decrease (in the order of magnitude) of ∼3.0 ± 0.6 was seen for the storms associated with sheath, followed by ∼2.7 ± 0.6 for EJ-S, ∼2.4 ± 0.55 for MC-S, ∼1.9 ± 0.4 for MC, and ∼1.6 ± 0.35 for EJ. At none of the times was the magnetopause pushed beyond 6.2 RE.

FIGURE 2

Figures 3A–H are in a similar format as Figures 2A–H, but for solar structures such as CME and CIR. From the figure, it can be seen that the flux decrease is more, with ∆F ≈ 2.2 ± 0.35 order of magnitude for the storms that are associated with CIR. The storms associated with CME show comparatively lesser flux decrease with ∆F ≈ 1.7 ± 0.41 order of magnitude, even though the Sym-H is high for CME-related storms.

FIGURE 3

A similar analysis was carried out for the storms that occurred during solar cycles 23 and 24, as shown in Figures 4A–H. It is in the same format as Figures 2, 3. Though the number of intense storms had decreased drastically, almost by ∼57% in solar cycle 24 when compared to solar cycle 23, no difference is seen in the level of electron flux decrease (Figure 4H). It is ∼1.69 ± 0.35 for solar cycle 23 and ∼1.77 ± 0.4 for solar cycle 24. However, it can be noticed that the overall flux level is significantly lower for the storms that occurred in solar cycle 24 than for those that occurred in solar cycle 23.

FIGURE 4

Effect of solar wind parameters

Some differences in maximum values of interplanetary conditions such as solar wind speed, pressure, density, and electric field are seen for different solar structures and substructures after performing epoch analysis, as seen in Figures 2, 3, respectively. Some previous studies had also examined the role of IMF Bz and solar wind dynamic pressure on radiation belt electron flux (Borovsky and Denton, 2010; Meredith et al., 2011; Yuan and Zong, 2013; Gao et al., 2015). Boynton et al. (2016)had carried out an error reduction ratio analysis and concluded that the solar wind dynamic pressure coupled with solar wind density are the main driving factors for the loss of electrons at energies 128 ≤ E ≤ 925 keV and the solar wind dynamic pressure coupled with southward IMF at energies 1.3 ≤ E ≤ 2 MeV at the geostationary orbits. We also tried to look at the role of solar wind dynamic pressure, speed, density, and electric field on flux depletions. The effect of IMF Bz is studied separately in the next section. We used maximum values of solar wind dynamic pressure, speed, density, and electric field obtained after epoch analysis to check its influence on the level of flux decrease described in terms of the order of magnitude, as shown in Figure 5 for different solar structures and substructures. Seen superimposed on it is an IMF Bz, which is divided into two groups, viz., IMF Bz < −20 nT (big circles) and IMF Bz > −20 nT (small circles). From the figure, it is evident that most of the flux depletion is accompanied by strong southward IMF Bz. All the CIR-related storms are produced by IMF Bz > −20 nT. It can also be seen that there is no significant difference in the values of Vmax, Nmax, Pmax, and Emax for the storms associated with different solar drivers. The average values of Vmax, Nmax, Pmax, and Emax along with flux decrease (∆F) for different solar drivers are given in Table 2. Figure 6 is similar to Figure 5, with R0 superimposed instead of IMF Bz. Here, R0 is categorized in two groups, viz., R0 < 6 (small circles) and R0 ≥ 6 (big circles). From the figure, it can be seen that in most of the cases, the magnetopause did not move inward beyond the geostationary orbit. This suggests that essentially, the flux decrease is governed by the ‘Dst effect’ (McIlwain, 1966). Having said that, one cannot neglect the effects of wave–particle interactions during such events. Table 3 shows the number of events for R0 < 6 RE and R0 ≥ 6 RE. It can be seen that during the storms that are associated with sheaths (MC-S, EJ-S, and S), mostly the magnetopause is pushed inward with R0 < 6. During such cases, the magnetopause shadowing effect may dominate. The sheath passages also favor ULF waves to grow and therefore deplete the particles under the influence of pitch angle scattering.

FIGURE 5

TABLE 2

TypeVmax (Km/s)Nmax (n/cc)Pmax (nPa)Emax (V/m)∆F (ord. of mag.)
MC521.715.537.3069.1131.2727
MC-S793.624.4627.122.481.8726
EJ577.216.6211.677.9961.0932
EJ-S640.437.8226.0915.971.5395
S656.523.817.7116.562.2656
CIR593.726.679.8186.191.5901

Average values of maximum solar wind speed (Vmax in km/s), density (Nmax in n/cc), dynamic pressure (Pmax in nPa), electric field (Emax in V/m), and electron flux decrease (∆F in the order of magnitude) for different solar drivers after performing epoch analysis.

FIGURE 6

TABLE 3

TypeR0 < 6R0 ≥ 6Total
MC63945
MC-S639
EJ101929
EJ-S325
S336
CIR189

Number of events with R0 < 6 and R0 ≥ 6 for different solar drivers.

Dependence of IMF Bz

Apart from solar wind parameters, IMF Bz has been observed to show peculiar features during electron flux depletions. Gao et al. (2015) have shown that the strong southward IMF Bz is solely capable of significant relativistic electron depletions. Figure 2 shows that in some cases, IMF Bz is seen to turn northward before turning southward during the course of flux decrease. To check the effect in detail, we plotted ∆F against IMF Bz for A) MC, B) MC-S, C) EJ, D) EJ-S, and E) S, as shown in Figure 7. The IMF Bz and flux values are of 1 min resolution and are mean values taken after performing epoch analysis during the course of flux depletion. From the figure, it can be noted that the storms that are associated with MC-S, EJ-S, and S show more positive IMF Bz values (fourth quadrant), for which the flux decrease is seen to be comparatively high. Also, we can see that the storms associated with these drivers have a minimum Bz exceeding −20 nT, whereas the storms associated with the other two categories have a minimum Bz < −15 nT. A similar trend is observed for storms triggered by CIR when compared to CME, as shown in Figure 8. Here also, the fourth quadrant for CIR-related storms is dominant, highlighting the importance of northward IMF Bz before turning southward. A similar analysis is carried out for the storms of both solar cycles (Figure 9). However, no difference is seen either for positive IMF Bz values or minimum IMF Bz between the two, which may have led to no significant change in the level of flux decrease.

FIGURE 7

FIGURE 8

FIGURE 9

Discussion

By performing epoch analysis on the interplanetary conditions and GOES electron flux data, we tried to examine the effect of different solar drivers on the loss of radiation belt electron flux at geostationary orbit during intense geomagnetic storms. Reeves et al. (2003) analyzed the response of relativistic electrons to 276 moderate and intense (Dst < −50 nT) geomagnetic storms. They observed that 56% of the storms showed an overall increase in the trapped flux, only 19% exhibited a decrease, while there was no flux change during 28% of the storms. This suggests the complexity in the response of relativistic electron flux to geomagnetic storms, and it is a delicate balance between acceleration and loss of the particles. As our focus was to analyze only the flux depletion and its dependence on various solar drivers, we chose the days of intense geomagnetic storms, which guaranteed only flux decrease. A total of 103 intense (Dst ≤ −100 nT) geomagnetic storms occurred during 1996–2019, which are considered in the present study, and the change in relativistic electron flux for E > 0.6 and > 0.8 MeV at geostationary orbit is observed using GOES electron flux measurements. A decrease of more than one order of magnitude is seen in the electron flux for all the events. The flux decrease is observed to start with the main phase of the geomagnetic storm. Many different mechanisms, right from the adiabatic process (“Dst effect”), magnetopause shadowing, and scattering of electrons into the loss cone by resonant wave–particle interaction, either alone or in combination act on these particles. There are numerous studies to find the exact mechanism behind electron flux depletion (Bortnik et al., 2006; Shprits et al., 2006; Kim et al., 2010; Turner et al., 2012; Turner et al., 2014; Yuan and Zong, 2013; Baker et al., 2016; Tsurutani et al., 2016; and references given in Millan and Thorne, 2007); however, very few studies have focused on the solar drivers and interplanetary conditions on facilitating electron depletions. In this study, we exclusively focus on the role of different solar structures, such as CME and CIR, and different substructures, such as magnetic cloud, magnetic cloud with sheath, ejecta, ejecta with sheath, and only sheath, in favoring the depletions. The space weather depends mainly on the condition of the Sun and its emissions that hit the Earth, thereby making it necessary to analyze any effect/process happening in the magnetosphere due to changes in solar drivers. As the radiation belt electron flux response is different for shocks, sheaths, and MCs, it is necessary to understand their short- and long-term effects along with their occurrence (Kilpua E. et al., 2017). We make use of superposed epoch analysis to see the effect of the aforementioned solar drivers on the radiation belt electron loss. Gopalswamy et al. (2010) found that the CMEs with magnetic cloud (MC) structure are more geoeffective than the ejecta (EJ). We also found a higher degree of flux depletion for MC-related storms than for those related to EJ. We observed (from Figure 2) more flux depletion in the case of storms that are related to sheaths (MC-S, EJ-S, and S) than for the ones which are not (MC and EJ). Yermolaev et al. (2010) found that the geoeffectiveness of MC with sheath was the highest at 61%, that for EJ with sheath was 21%, and for the one without sheath had the lowest geoeffectiveness—only about 8%. The remaining contribution comes from only sheath and CIR-related storms. The sheath properties, which include high dynamic pressure (Palmroth et al., 2007; Myllys et al., 2016), enhanced ULF wave power in turn enhancing the viscous interactions at the magnetosphere (Borovsky and Funsten, 2003), and also stronger compression of the plasma and field caused by high Alfven Mach numbers (Borovsky and Brin, 2014; Myllys et al., 2016) all positively contribute toward the solar wind–magnetosphere coupling (Klipua et al., 2017b). However, the total energy input into the magnetosphere is larger during ICMEs without sheath due to their long encounters. The strong depleting tendency of the sheath-associated storms are presented in Figure 2 that may come from the pitch angle scattering and radial diffusion in combination with the highly compressed dayside magnetopause, due to enhanced ULF power and high dynamic pressure.

Though the storms associated with CME have been observed to be more geoeffective than the storms associated with CIR, we found that the radiation belt electron depletion is more in the latter case (Figure 3). Turner et al. (2019) observed enhancements of MeV electrons at higher L-shells (L > 4.5) after the initial depletion during the main phase of the storm. They also observed higher flux depletions for CME-related storms. However, our results contradict both these observations. We see a comparatively higher flux decrease for CIR-related storms. Also, we do not observe any flux enhancements after the initial depletion. Miyoshi and Kataoka (2005), after applying the superposed epoch analysis, also found that the CIRs tend to cause a much higher increase in the flux than ICMEs at the geosynchronous orbits. Benacquista et al. (2018) also supported the idea of flux increase on a large range of L* and decrease by only a limited number of CIR storms. Koskinen and Kilpua (2022) supported the idea of relativistic flux decrease during SIRs. The observations shown here are strictly during intense geomagnetic storms. Our results urge a reinvestigation of the comparison of flux decrease during CME- and CIR-driven intense geomagnetic storms.

We did not find any significant change in the level of flux decrease for the storms that occurred during the two solar cycles 23 and 24 (Figure 4), although the occurrence of intense geomagnetic storms had drastically decreased in solar cycle 24 (Figure 1). Selvakumaran et al. (2016) from their study on the comparison of moderate geomagnetic storms during solar cycles 23 and 24 observed a reduced magnetospheric energy transfer during solar cycle 24. Gopalswamy et al. (2015) from their study on the properties and geoeffectiveness of magnetic clouds during solar cycles 23 and 24 concluded that the geoeffectiveness was comparatively reduced during solar cycle 24 because of the anomalous CME expansion through its course in the interplanetary medium. Our results from Figure 4 show that the reduced geoefficiency or reduced magnetospheric energy transfer in solar cycle 24 has very less or no impact on the dynamics of radiation belt electron flux depletions.

The interplanetary and solar wind conditions also play an important role in causing radiation belt energetic electron flux decrease. We tried to understand the variations in the degree of flux decrease with different interplanetary properties such as solar wind pressure, speed, density, and electric field as shown in Figure 5 (which includes IMF Bz) and Figure 6 (which includes magnetopause distance). The high flux decrease is seen for the events when IMF Bz is < −20 nT. In most of the cases, the magnetopause did not cross the geostationary orbit, eliminating the possibility of magnetopause shadowing. For CIR-related storms, the influence of IMF Bz being comparatively less and R0 ≥ 6 suggest the importance of wave–particle interaction-driven pitch angle scattering as a cause for the flux decrease. As mentioned earlier, here the magnetopause distance is calculated using Shue et al. (1997) model. This model is widely and effectively used by many researchers like Turner et al. (2012), Gao et al. (2015), and Herrera et al. (2016). But, it should be kept in mind that the model values can have uncertainties and can vary from the actual values. Recently, Staples et al. (2020) constructed a database of ∼20,000 spacecraft crossings of the dayside magnetopause and concluded that when the magnetopause is compressed below 8 RE, the average measured location is >1 RE inside the magnetopause. They also suggested that even extreme magnetopause events rarely reach the outer radiation belt. Our result that the magnetopause does not move beyond the geostationary orbit (∼6 RE) is in-line with the conclusions drawn by Staples et al. (2020). The solar wind pressure and speed seem to have an almost similar effect on the flux decrease. Previous studies have only focused on the role of solar wind dynamic pressure, IMF Bz, and, up to some extent, solar wind speed. From their study on the correlation between relativistic electrons at GEO and properties of solar wind drivers during the solar minimum period, Blake et al. (1997) found that solar wind speed and density increase along with the southward turning of IMF leading to the enhancement of relativistic electrons. Many other studies have also found a positive correlation between the relativistic flux and solar wind speed (Baker et al., 1979; Paulika and Blake, 1979). Li et al. (2001) found solar wind speed to be the most important factor in their prediction model of electron fluxes at geostationary orbits. Some other studies have favored the role of high solar wind dynamic pressure and southward IMF Bz in reducing the relativistic electrons in the outer radiation belt (Borovsky and Denton, 2010; Meredith et al., 2011; Yuan and Zong, 2013; Gao et al., 2015).

The role of IMF Bz in the depletion of electron flux is analyzed separately as can be seen from Figures 7, 8, 9. We found two distinct features: 1) the flux decrease is more when there are more positive IMF Bz values and 2) the flux decrease is also more when the minimum negative Bz value is comparatively lesser. These two features are true for the cases of MC-S, EJ-S, S (Figures 7B,D,E), and CIR (Figure 8). Both of the features are absent in the case of comparison between solar cycles 23 and 24 where we do not observe much difference between the level of the flux. Gao et al. (2015), by analyzing the electron flux dropout events during storm and non-storm periods, found that when IMF Bz was southward, both the flux of precipitating electrons and the ratio between the precipitating electrons and trapped electrons were much larger. Our results show that the northward turning of IMF Bz before southward contributes positively toward more flux decrease. This can be visualized in the following way: during the course of positive Bz, the magnetosphere gets compressed and triggers the diffusion of the electrons to higher L-shells. Once the Bz turns southward, the magnetopause becomes eroded significantly due to enhanced magnetic reconnection. Souza et al. (2017) have studied the recovery of the relativistic radiation belt electrons and argue that the whistler mode chorus wave power is enhanced when IMF Bz is negative, on average, which in addition to amplification of magnetic integrated power in the ULF range accelerates the outer radiation belt electrons. Our study deals with the depletion of the electrons and suggests that the flux decrease is strengthened when IMF Bz turns southward after a significant positive course. Gao et al. (2015) suggested that the more stretched magnetic field during large solar wind dynamic pressure or southward IMF Bz intensifies the ring current. Then, the relativistic electrons are scattered as a result of deviation of the first adiabatic invariant. Our study not only stresses the importance of southward IMF Bz but also gives insight into the northward turning of IMF Bz before turning southward during a geomagnetic storm. We also suggest that the lesser negative Bz minimum leads to more flux decrease which can be attributed to maximum energy transfer during lesser southward IMF Bz (Selvakumaran et al., 2016).

By studying the depleting effects of ICME-driven sheath regions on the outer electron radiation belt, Hietela et al. (2014) suggested that under magnetospheric compression, the sheaths increase the radial diffusion that enhances the chances of magnetopause shadowing effects producing higher flux decrease. It is also believed that the fluctuating IMF Bz can launch magnetosonic waves, which propagate into the magnetosphere and can scatter the electrons into the loss cone by virtue of the resonant wave–particle interaction. Kilpua E. et al. (2017) has also claimed the dominating tendency of sheath passages in depleting the electrons. The results presented in this study suggest the importance of considering solar driver properties while anticipating the electron flux changes in the radiation belts. The detailed analysis of electron flux decrease at different L-shells using long-term data will be pursued in the future to add to the knowledge gained.

Summary and conclusion

A superposed epoch analysis is performed to investigate the effect of different solar structures and substructures on the depletion of relativistic electron flux at the geostationary orbit during the cases of intense geomagnetic storms. Our analysis found some interesting results:

  • 1) Sheath-related storms (MC-S, EJ-S, and S) produce more flux decrease than the non-sheath ones (MC and EJ).

  • 2) The increase in the solar wind pressure and speed increases the flux decrease.

  • 3) Either northward IMF Bz before turning southward or rapidly fluctuating IMF Bz causes a higher flux decrease.

As the main aim of space weather studies is to know what, when, and how it will happen, our results presented here may provide a positive input to radiation belt modeling studies, while predicting the dynamics under particular solar and solar wind conditions.

Statements

Data availability statement

Publicly available data sets were analyzed in this study. These data can be found at OMNIWeb (https://omniweb.gsfc.nasa.gov/form/dx1.html), World Data Center, Kyoto (https://wdc.kugi.kyoto-u.ac.jp/dst_final/index.html), GOES (https://www.ngdc.noaa.gov/stp/satellite/goes/dataaccess.html), and CDAWeb (https://cdaweb.gsfc.nasa.gov).

Author contributions

SG, the first author has conceptualized the idea, carried out the analysis, written the manuscript, and contributed towards the physical interpretation of the results. DH has contributed towards interpreting the results and also provided the basic infrastructure to carry out the research. RS has identified the solar structures and substructures and contributed in interpreting the results. TP has contributed towards interpreting the results.

Funding

This work is partly supported by the National Natural Science Foundation of China (42050410313, 42030101, and 41974185). SG carried out this work using the research grant from the Science and Engineering Research Board, Department of Science and Technology, India (2020/RJF/000125). RS acknowledges the support from the research grant from the Science and Engineering Research Board, Department of Science and Technology, India (PDF/2021/002226).

Acknowledgments

The authors thank the head of the School of Ocean and Earth Sciences for supporting the research work. They also thank SPL and VSSC for encouraging the research activities toward this work and the OMNIWeb (https://omniweb.gsfc.nasa.gov/form/dx1.html) team for providing solar wind data. They also thank the World Data Center, Kyoto, for providing Dst values (https://wdc.kugi.kyoto-u.ac.jp/dst_final/index.html), GOES (https://www.ngdc.noaa.gov/stp/satellite/goes/dataaccess.html) team, and CDAWeb (https://cdaweb.gsfc.nasa.gov).

Conflict of interest

The authors declare that the research was conducted in the absence of any commercial or financial relationships that could be construed as a potential conflict of interest.

Publisher’s note

All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, editors, and reviewers. Any product that may be evaluated in this article, or claim that may be made by its manufacturer, is not guaranteed or endorsed by the publisher.

References

  • 1

    AllenJ. H. (2002). “Historical and recent solar activity and geomagnetic storms affecting spacecraft operations,” in Proceedings of the government Microcircuit and applications conference (Monterey, CA: GOMAC’02).

  • 2

    BakerD. N.BelianR. D.HigbieP. R.KlebesadelR. W.BlakeJ. B. (1987). Deep dielectric charging effects due to high-energy electrons in Earth's outer magnetosphere. J. Electrost.20 (1), 319. 10.1016/0304-3886(87)90082-9

  • 3

    BakerD. N.EricksonP. J.FennellJ. F.FosterJ. C.JaynesA. N.VerronenP. T. (2018). Space weather effects in the Earth’s radiation belts. Space Sci. Rev.214 (1), 1760. 10.1007/s11214-017-0452-7

  • 4

    BakerD. N.HigbieP. R.BelianR. D.HonesE. W.Jr (1979). Do Jovian electrons influence the terrestrial outer radiation zone?Geophys. Res. Lett.6 (6), 531534. 10.1029/gl006i006p00531

  • 5

    BakerD. N.JaynesA. N.KanekalS. G.FosterJ. C.EricksonP. J.FennellJ. F.et al (2016). Highly relativistic radiation belt electron acceleration, transport, and loss: Large solar storm events of March and June 2015. JGR. Space Phys.121 (7), 66476660. 10.1002/2016ja022502

  • 6

    BakerD. N.KanekalS. G.BlakeJ. B. (2004). Characterizing the Earth's outer Van Allen zone using a radiation belt content index. Space weather.2 (2). 10.1029/2003sw000026

  • 7

    BakerD. N.KanekalS. G.HorneR. B.MeredithN. P.GlauertS. A. (2007). Low‐altitude measurements of 2–6 MeV electron trapping lifetimes at 1.5≤ L≤ 2.5. Geophys. Res. Lett.34 (20), L20110. 10.1029/2007gl031007

  • 8

    BenacquistaR.BoscherD.RochelS.MagetV. (2018). Variations of the electron fluxes in the terrestrial radiation belts due to the impact of corotating interaction regions and interplanetary coronal mass ejections. J. Geophys. Res. Space Phys.123 (2), 11911199. 10.1002/2017ja024796

  • 9

    BlakeJ. B.BakerD. N.TurnerN.OgilvieK. W.LeppingR. P. (1997). Correlation of changes in the outer‐zone relativistic‐electron population with upstream solar wind and magnetic field measurements. Geophys. Res. Lett.24 (8), 927929. 10.1029/97gl00859

  • 10

    BorovskyJ. E.BirnJ. (2014). The solar wind electric field does not control the dayside reconnection rate. J. Geophys. Res. Space Phys.119 (2), 751760. 10.1002/2013ja019193

  • 11

    BorovskyJ. E.DentonM. H. (2010). Magnetic field at geosynchronous orbit during high‐speed stream‐driven storms: Connections to the solar wind, the plasma sheet, and the outer electron radiation belt. J. Geophys. Res.115 (A8). 10.1029/2009ja015116

  • 12

    BorovskyJ. E.FunstenH. O. (2003). MHD turbulence in the Earth's plasma sheet: Dynamics, dissipation, and driving. J. Geophys. Res.108 (A7), 1284. 10.1029/2002ja009625

  • 13

    BortnikJ.ThorneR. M.O'BrienT. P.GreenJ. C.StrangewayR. J.ShpritsY. Y.et al (2006). Observation of two distinct, rapid loss mechanisms during the 20 November 2003 radiation belt dropout event. J. Geophys. Res.111 (A12), A12216. 10.1029/2006ja011802

  • 14

    BoyntonR. J.MourenasD.BalikhinM. A. (2016). Electron flux dropouts at Geostationary Earth Orbit: Occurrences, magnitudes, and main driving factors. J. Geophys. Res. Space Phys.121 (9), 84488461. 10.1002/2016ja022916

  • 15

    BoyntonR. J.MourenasD.BalikhinM. A. (2017). Electron flux dropouts at L∼ 4.2 from global positioning system satellites: Occurrences, magnitudes, and main driving factors. J. Geophys. Res. Space Phys.122 (11), 11428. 10.1002/2017ja024523

  • 16

    ClilverdM. A.RodgerC. J.AnderssonM. E.SeppalaA.VerronenP. T. (2016). “Linkages between the radiation belts, polar atmosphere and climate: Electron precipitation through wave particle interactions,” in Waves particles and storms in geospace (Oxford: Oxford University Press), 354376.

  • 17

    ElkingtonS. R.HudsonM. K.ChanA. A. (2003). Resonant acceleration and diffusion of outer zone electrons in an asymmetric geomagnetic field. J. Geophys. Res.108 (A3), 1116. 10.1029/2001ja009202

  • 18

    FriedelR. H. W.ReevesG. D.ObaraT. (2002). Relativistic electron dynamics in the inner magnetosphere—a review. J. Atmos. Solar-Terrestrial Phys.64 (2), 265282. 10.1016/s1364-6826(01)00088-8

  • 19

    GaoX.LiW.BortnikJ.ThorneR. M.LuQ.MaQ.et al (2015). The effect of different solar wind parameters upon significant relativistic electron flux dropouts in the magnetosphere. JGR. Space Phys.120 (6), 43244337. 10.1002/2015ja021182

  • 20

    GopalswamyN.YashiroS.MichalekG.XieH.MäkeläP.VourlidasA.et al (2010). A catalog of halo coronal mass ejections from SOHO. Sun Geosph.5 (1), 716.

  • 21

    GopalswamyN.YashiroS.XieH.AkiyamaS.MäkeläP. (2015). Properties and geoeffectiveness of magnetic clouds during solar cycles 23 and 24. JGR. Space Phys.120 (11), 92219245. 10.1002/2015ja021446

  • 22

    GreenJ. C.OnsagerT. G.O'BrienT. P.BakerD. N. (2004). Testing loss mechanisms capable of rapidly depleting relativistic electron flux in the Earth's outer radiation belt. J. Geophys. Res.109 (A12), A12211. 10.1029/2004ja010579

  • 23

    HerreraD.MagetV. F.Sicard PietA. (2016). Characterizing magnetopause shadowing effects in the outer electron radiation belt during geomagnetic storms. JGR. Space Phys.121 (10), 95179530. 10.1002/2016ja022825

  • 24

    HietalaH.KilpuaE. K. J.TurnerD. L.AngelopoulosV. (2014). Depleting effects of ICME‐driven sheath regions on the outer electron radiation belt. Geophys. Res. Lett.41 (7), 22582265. 10.1002/2014gl059551

  • 25

    HorneR. B.ThorneR. M.GlauertS. A.AlbertJ. M.MeredithN. P.AndersonR. R. (2005). Timescale for radiation belt electron acceleration by whistler mode chorus waves. J. Geophys. Res.110 (A3), A03225. 10.1029/2004ja010811

  • 26

    IlesR. H. A.FazakerleyA. N.JohnstoneA. D.MeredithN. P.BühlerP. (2002). The relativistic electron response in the outer radiation belt during magnetic storms. Ann. Geophys.20, 957965. 10.5194/angeo-20-957-2002

  • 27

    KilpuaE. K. J.BaloghA.Von SteigerR.LiuY. D. (2017b). Geoeffective properties of solar transients and stream interaction regions. Space Sci. Rev.212 (3), 12711314. 10.1007/s11214-017-0411-3

  • 28

    KilpuaE. K. J.HietalaH.TurnerD. L.KoskinenH. E. J.PulkkinenT. I.RodriguezJ. V.et al (2015). Unraveling the drivers of the storm time radiation belt response. Geophys. Res. Lett.42 (9), 30763084. 10.1002/2015gl063542

  • 29

    KilpuaE.KoskinenH. E.PulkkinenT. I. (2017a). Coronal mass ejections and their sheath regions in interplanetary space. Living Rev. Sol. Phys.14 (1), 583. 10.1007/s41116-017-0009-6

  • 30

    KimH. J.ChanA. A. (1997). Fully adiabatic changes in storm time relativistic electron fluxes. J. Geophys. Res.102 (A10), 2210722116. 10.1029/97ja01814

  • 31

    KimK. C.LeeD. Y.KimH. J.LeeE. S.ChoiC. R. (2010). Numerical estimates of drift loss and Dst effect for outer radiation belt relativistic electrons with arbitrary pitch angle. J. Geophys. Res.115 (A3). 10.1029/2009ja014523

  • 32

    KoskinenH. E.KilpuaE. K. (2022). Physics of Earth’s radiation belts: Theory and observations. Springer Nature, 272.

  • 33

    LiX.BakerD. N.TemerinM.CaytonT. E.ReevesE. G. D.ChristensenR. A.et al (1997). Multisatellite observations of the outer zone electron variation during the November 3–4, 1993, magnetic storm. J. Geophys. Res.102 (A7), 1412314140. 10.1029/97ja01101

  • 34

    LiX.TemerinM.BakerD. N.ReevesG. D.LarsonD. (2001). Quantitative prediction of radiation belt electrons at geostationary orbit based on solar wind measurements. Geophys. Res. Lett.28 (9), 18871890. 10.1029/2000gl012681

  • 35

    LyonsL. R.ThorneR. M. (1973). Equilibrium structure of radiation belt electrons. J. Geophys. Res.78 (13), 21422149. 10.1029/ja078i013p02142

  • 36

    McIlwainC. E. (1966). Ring current effects on trapped particles. J. Geophys. Res.71 (15), 36233628. 10.1029/jz071i015p03623

  • 37

    MeredithN. P.CainM.HorneR. B.ThorneR. M.SummersD.AndersonR. R. (2003). Evidence for chorus‐driven electron acceleration to relativistic energies from a survey of geomagnetically disturbed periods. J. Geophys. Res.108 (A6), 1248. 10.1029/2002ja009764

  • 38

    MeredithN. P.HorneR. B.LamM. M.DentonM. H.BorovskyJ. E.GreenJ. C. (2011). Energetic electron precipitation during high‐speed solar wind stream driven storms. J. Geophys. Res.116 (A5). 10.1029/2010ja016293

  • 39

    MillanR. M.ThorneR. (2007). Review of radiation belt relativistic electron losses. J. Atmos. Solar-Terrestrial Phys.69 (3), 362377. 10.1016/j.jastp.2006.06.019

  • 40

    MiyoshiY.KataokaR. (2005). Ring current ions and radiation belt electrons during geomagnetic storms driven by coronal mass ejections and corotating interaction regions. Geophys. Res. Lett.32 (21), L21105. 10.1029/2005gl024590

  • 41

    MyllysM.KilpuaE. K. J.LavraudB.PulkkinenT. I. (2016). Solar wind‐magnetosphere coupling efficiency during ejecta and sheath‐driven geomagnetic storms. J. Geophys. Res. Space Phys.121 (5), 43784396. 10.1002/2016ja022407

  • 42

    NiB.XiangZ.GuX.ShpritsY. Y.ZhouC.ZhaoZ.et al (2016). Dynamic responses of the Earth's radiation belts during periods of solar wind dynamic pressure pulse based on normalized superposed epoch analysis. J. Geophys. Res. Space Phys.121 (9), 85238536. 10.1002/2016ja023067

  • 43

    OnsagerT. G.RostokerG.KimH. J.ReevesG. D.ObaraT.SingerH. J.et al (2002). Radiation belt electron flux dropouts: Local time, radial, and particle‐energy dependence. J. Geophys. Res.107 (A11), 138221. 10.1029/2001ja000187

  • 44

    PalmrothM.PartamiesN.PolviJ.PulkkinenT. I.McComasD. J.BarnesR. J.et al (2007). Solar wind–magnetosphere coupling efficiency for solar wind pressure impulses. Geophys. Res. Lett.34 (11), L11101. 10.1029/2006gl029059

  • 45

    PaulikasG. A.BlakeJ. B. (1979). Effects of the solar wind on magnetospheric dynamics: Energetic electrons at the synchronous orbit. Quantitative Model. Magnetos. Process. Geophys. Monogr. Ser21, 180202.

  • 46

    PhamK. H.TuW.XiangZ. (2017). Quantifying the precipitation loss of radiation belt electrons during a rapid dropout event. JGR. Space Phys.122 (10), 10287. 10.1002/2017ja024519

  • 47

    PintoV. A.KimH. J.LyonsL. R.BortnikJ. (2018). Interplanetary parameters leading to relativistic electron enhancement and persistent depletion events at geosynchronous orbit and potential for prediction. JGR. Space Phys.123 (2), 11341145. 10.1002/2017ja024902

  • 48

    ReevesG. D.McAdamsK. L.FriedelR. H. W.O'brienT. P. (2003). Acceleration and loss of relativistic electrons during geomagnetic storms. Geophys. Res. Lett.30 (10). 10.1029/2002gl016513

  • 49

    ReevesG. D.SpenceH. E.HendersonM. G.MorleyS. K.FriedelR. H. W.FunstenH. O.et al (2013). Electron acceleration in the heart of the Van Allen radiation belts. Science341 (6149), 991994. 10.1126/science.1237743

  • 50

    RichardsonI. G.CaneH. V. (2010). Near-Earth interplanetary coronal mass ejections during solar cycle 23 (1996–2009): Catalog and summary of properties. Sol. Phys.264 (1), 189237. 10.1007/s11207-010-9568-6

  • 51

    SelvakumaranR.VeenadhariB.AkiyamaS.PandyaM.GopalswamyN.YashiroS.et al (2016). On the reduced geoeffectiveness of solar cycle 24: A moderate storm perspective. J. Geophys. Res. Space Phys.121 (9), 81888202. 10.1002/2016ja022885

  • 52

    ShpritsY. Y.DrozdovA. Y.SpasojevicM.KellermanA. C.UsanovaM. E.EngebretsonM. J.et al (2016). Wave-induced loss of ultra-relativistic electrons in the Van Allen radiation belts. Nat. Commun.7 (1), 1288312887. 10.1038/ncomms12883

  • 53

    ShpritsY. Y.ThorneR. M.FriedelR.ReevesG. D.FennellJ.BakerD. N.et al (2006). Outward radial diffusion driven by losses at magnetopause. J. Geophys. Res.111 (A11), A11214. 10.1029/2006ja011657

  • 54

    ShueJ. H.ChaoJ. K.FuH. C.RussellC. T.SongP.KhuranaK. K.et al (1997). A new functional form to study the solar wind control of the magnetopause size and shape. J. Geophys. Res.102 (A5), 94979511. 10.1029/97ja00196

  • 55

    SouzaV. M.LopezR. E.JauerP. R.SibeckD. G.PhamK.Da SilvaL. A.et al (2017). Acceleration of radiation belt electrons and the role of the average interplanetary magnetic field Bz component in high‐speed streams. J. Geophys. Res. Space Phys.122 (10), 10084.

  • 56

    StaplesF. A.RaeI. J.ForsythC.SmithA. R. A.MurphyK. R.RaymerK. M.et al (2020). Do statistical models capture the dynamics of the magnetopause during sudden magnetospheric compressions?J. Geophys. Res. Space Phys.125 (4), e2019JA027289. 10.1029/2019ja027289

  • 57

    SummersD.ThorneR. M.XiaoF. (1998). Relativistic theory of wave‐particle resonant diffusion with application to electron acceleration in the magnetosphere. J. Geophys. Res.103 (A9), 2048720500. 10.1029/98ja01740

  • 58

    ThorneR. M.KennelC. (1971). Relativistic electron precipitation during magnetic storm main phase. J. Geophys. Res.76 (19), 44464453. 10.1029/ja076i019p04446

  • 59

    TsurutaniB. T.HajraR.TanimoriT.TakadaA.RemyaB.MannucciA. J.et al (2016). Heliospheric plasma sheet (HPS) impingement onto the magnetosphere as a cause of relativistic electron dropouts (REDs) via coherent EMIC wave scattering with possible consequences for climate change mechanisms. J. Geophys. Res. Space Phys.121 (10), 10130. 10.1002/2016ja022499

  • 60

    TurnerD. L.AngelopoulosV.LiW.BortnikJ.NiB.MaQ.et al (2014). Competing source and loss mechanisms due to wave‐particle interactions in Earth's outer radiation belt during the 30 September to 3 October 2012 geomagnetic storm. JGR. Space Phys.119 (3), 19601979. 10.1002/2014ja019770

  • 61

    TurnerD. L.KilpuaE. K. J.HietalaH.ClaudepierreS. G.O'BrienT. P.FennellJ. F.et al (2019). The response of Earth's electron radiation belts to geomagnetic storms: Statistics from the Van Allen Probes era including effects from different storm drivers. JGR. Space Phys.124 (2), 10131034. 10.1029/2018ja026066

  • 62

    TurnerD. L.ShpritsY.HartingerM.AngelopoulosV. (2012). Explaining sudden losses of outer radiation belt electrons during geomagnetic storms. Nat. Phys.8 (3), 208212. 10.1038/nphys2185

  • 63

    XiangZ.TuW.LiX.NiB.MorleyS. K.BakerD. N. (2017). Understanding the mechanisms of radiation belt dropouts observed by Van Allen Probes. JGR. Space Phys.122 (10), 98589879. 10.1002/2017ja024487

  • 64

    YermolaevY. I.NikolaevaN. S.LodkinaI. G.YermolaevM. Y. (2010). Specific interplanetary conditions for CIR-Sheath-and ICME-induced geomagnetic storms obtained by double superposed epoch analysis. Ann. Geophys.28, 21772186. 10.5194/angeo-28-2177-2010

  • 65

    YuanC.ZongQ. (2013). Relativistic electron fluxes dropout in the outer radiation belt under different solar wind conditions. J. Geophys. Res. Space Phys.118 (12), 75457556. 10.1002/2013ja019066

  • 66

    YueC.ZongQ. (2011). Solar wind parameters and geomagnetic indices for four different interplanetary shock/ICME structures. J. Geophys. Res.116 (A12). 10.1029/2011ja017013

  • 67

    ZhangX. J.LiW.ThorneR. M.AngelopoulosV.MaQ.LiJ.et al (2016). Physical mechanism causing rapid changes in ultrarelativistic electron pitch angle distributions right after a shock arrival: Evaluation of an electron dropout event. JGR. Space Phys.121 (9), 83008316. 10.1002/2016ja022517

Summary

Keywords

radiation belt, solar wind, solar drivers, geomagnetic storms, electron flux depletion

Citation

Gokani SA, Han D-S, Selvakumaran R and Pant TK (2022) Dependence of radiation belt flux depletions at geostationary orbit on different solar drivers during intense geomagnetic storms. Front. Astron. Space Sci. 9:952486. doi: 10.3389/fspas.2022.952486

Received

25 May 2022

Accepted

07 October 2022

Published

21 October 2022

Volume

9 - 2022

Edited by

Joseph E. Borovsky, Space Science Institute, United States

Reviewed by

Richard Boynton, The University of Sheffield, United Kingdom

Chongjing Yuan, Institute of Geology and Geophysics (CAS), China

Updates

Copyright

*Correspondence: Sneha A. Gokani,

This article was submittedto Space Physics, a section of the journal Frontiers in Astronomy andSpace Sciences

Disclaimer

All claims expressed in this article are solely those of the authors and do not necessarily represent those of their affiliated organizations, or those of the publisher, the editors and the reviewers. Any product that may be evaluated in this article or claim that may be made by its manufacturer is not guaranteed or endorsed by the publisher.

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