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Is the High-Resolution Coronal Imager Resolving Coronal Strands? Results from AR 12712

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Published 2020 April 7 © 2020 The Author(s). Published by the American Astronomical Society.
, , Citation Thomas Williams et al 2020 ApJ 892 134 DOI 10.3847/1538-4357/ab6dcf

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0004-637X/892/2/134

Abstract

Following the success of the first mission, the High-Resolution Coronal Imager (Hi-C) was launched for a third time (Hi-C 2.1) on 2018 May 29 from the White Sands Missile Range, NM, USA. On this occasion, 329 s of 17.2 nm data of target active region AR 12712 were captured with a cadence of ≈4 s, and a plate scale of 0farcs129 pixel−1. Using data captured by Hi-C 2.1 and co-aligned observations from SDO/AIA 17.1 nm, we investigate the widths of 49 coronal strands. We search for evidence of substructure within the strands that is not detected by AIA, and further consider whether these strands are fully resolved by Hi-C 2.1. With the aid of multi-scale Gaussian normalization, strands from a region of low emission that can only be visualized against the contrast of the darker, underlying moss are studied. A comparison is made between these low-emission strands and those from regions of higher emission within the target active region. It is found that Hi-C 2.1 can resolve individual strands as small as ≈202 km, though the more typical strand widths seen are ≈513 km. For coronal strands within the region of low emission, the most likely width is significantly narrower than the high-emission strands at ≈388 km. This places the low-emission coronal strands beneath the resolving capabilities of SDO/AIA, highlighting the need for a permanent solar observatory with the resolving power of Hi-C.

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1. Introduction

The NASA sounding rocket, Hi-C, was first launched on 2012 July 11 and it captured high-resolution (≈0farcs3–0farcs4), high-cadence (≈5 s) images of active region 11520 (Kobayashi et al. 2014) in a narrowband 19.3 nm channel. The unprecedented capabilities of this instrument allowed the corona to be viewed in greater detail than previously possible with spaceborne instruments, e.g., the Solar Dynamics Observatory/Atmospheric Imaging Assembly (SDO/AIA) (1farcs5, 12 s; Lemen et al. 2012) and Solar and Heliospheric Observatory (SOHO)/EIT (5'', 12 minutes; Delaboudinière et al. 1995). Studies on the data obtained during the maiden flight of Hi-C revealed new information on the small-scale structures in the corona and transition region. Several publications have resulted from those five minutes of observations, including energy release along braided structures (Cirtain et al. 2013; Tiwari et al. 2014; Thalmann et al. 2014; Pontin et al. 2017), possible nanoflare heating in active-region moss (Testa et al. 2013; Winebarger et al. 2013), coronal loop structure (Peter et al. 2013; Aschwanden & Peter 2017; Barczynski et al. 2017), and counter-streaming along filament channels (Alexander et al. 2013).

Coronal loops form one of the basic building blocks of the corona because they exist both in the quiet Sun and in active regions. Observational investigation of their structure has taken place since the 1940s (Bray et al. 1991) with the loops viewed in the extreme ultraviolet (EUV) and X-ray channels. For active regions, there are two loop types that have predominantly been studied: the short, hot loops in the core of an active region, typically observed in X-rays, and the cooler, longer loops that surround the core, typically observed in EUV (Reale 2010). EUV loops are observed to evolve and cool. They are relatively steady over periods of several hours (Antiochos et al. 2003; Warren et al. 2010, 2011). In comparison, active-region core loops are hotter, shorter, and found in areas of strong magnetic field within an active region (Berger et al. 1999). Typically, coronal loops have lengths of the same order as the barometric scale height, though there are suggestions of miniature loops in the chromosphere that span just a single granule (Feldman 1983; Peter et al. 2013; Barczynski et al. 2017).

When studying the heating of coronal loops, one of the most important factors for consideration is whether the observed loop structure is isothermal or multi-thermal along the line of sight. If an observed loop is isothermal, it could indicate that the loop structure is being resolved by the imager/spectrometer, or, if there is substructure below the instrumental resolving limit, that the strands making up the loop are behaving coherently. Similarly, if a loop with no apparent structuring was observed to be multi-thermal then this could be a clear indicator that the loop consists of unresolved strands or that there are many other structures over a range of temperature along the line of sight. Thus, determining any resolved fundamental spatial scale or the presence of subelements within a loop is an important step in addressing how coronal loop (or strand) plasma is possibly being heated.

In an attempt to answer this fundamental question, Schmelz et al. (2001) constructed multi-thermal differential emission measures (DEMs) using SOHO/CDS and Yohkoh/SXT. The obtained temperature distributions were found to be inconsistent with isothermal plasma, along both the line of sight and the length of the loop. The advent of TRACE (Transition Region and Coronal Explorer; Handy et al. 1999) yielded more observations of the temperature profiles of coronal loops (Schmelz 2002; Winebarger et al. 2002, 2003; Cirtain et al. 2007; Schmelz et al. 2009; Tripathi et al. 2009). Work by Mulu-Moore et al. (2011) investigated eight active-region loops that were previously found to be isothermal (Aschwanden & Nightingale 2005). Using the ratio of cooling time to loop lifetime during the rising and decaying phases of the loops, they deduce that observed lifetimes are longer than expected for seven of the loops, suggesting that the loops are composed of sub-resolution strands and that many TRACE loops are actually unresolved. Warren et al. (2002) demonstrate that an impulsively heated loop bundle cools through the TRACE passbands, and propose that each strand could appear as a single, long-lived loop with flat 19.5/17.1 nm filter ratios due to the sequential heating of the strands. They argue that the model could reproduce observed downflows (Winebarger et al. 2002) and the broad DEM distribution along the loops (Schmelz et al. 2001). Similarly, other models have investigated the many-stranded nature of coronal loops and the impulsive heating through nanoflare events (Cargill & Klimchuk 2004; Sarkar & Walsh 2008, 2009; Taroyan et al. 2011; Price & Taroyan 2015).

More recently, high-resolution observations from instruments such as Hi-C and Interface Region Imaging Spectrograph (IRIS; De Pontieu et al. 2014) have weighed-in on the discussion of loop widths. For small loops (length < 1 Mm) Peter et al. (2013) find widths below 200 km, compared to 1450–2175 km for loops longer than 50 Mm, with no obvious signs of substructure present in the Hi-C data when compared with AIA. From this Peter et al. (2013) deduce that sub-resolution strands would have to be of the order 15 km wide or smaller for a 1500 km wide loop whose density and temperature vary smoothly across the structure. Brooks et al. (2013) investigate 91 coronal loops and suggest they are often structured at a scale of several hundred kilometers, ranging between 212 and 2291 km, with the most frequently occurring FWHM ≈ 640 km.

Further work on this by Brooks et al. (2016) combines IRIS observations and HYDRAD modeling (Bradshaw & Cargill 2013) to investigate 108 transition region loops whose FWHM ranges between 266 and 386 km. They argue that at these spatial scales the structures appear to be composed of monolithic stands rather than multi-stranded bundles.

Similarly, Aschwanden & Peter (2017) combine Monte Carlo simulations of EUV images with the OCCULT-2 loop detection algorithm on the first Hi-C data set. They find a most frequent distribution of ≈550 km for 105 measurements of loop width. From this, Aschwanden & Peter (2017) deduce that Hi-C is fully resolving the loop structures. However, when they compare the co-spatial results from AIA they find that AIA can only partially resolve loops ≳420 km.

The advancements made in high-resolution measurements of coronal loops, particularly by Brooks et al. (2016) and Aschwanden & Peter (2017), appear to highlight evidence that current instrumentation is at a stage of resolving individual plasma strands within the corona and hence provides some possible constraint on the heat input required for these features. A summary of measurements of coronal loop width can be found in Section 5.4.4 of Aschwanden (2004), along with a table of widths from 52 studies in Aschwanden & Peter (2017).

This paper undertakes a further examination of loop or strand widths but employs the new data set obtained from the flight of Hi-C 2.1 (Section 2). Using this unique data set, we ask whether Hi-C 2.1 is resolving individual coronal strands and what are their spatial scales? To answer this, five regions are investigated from the target active region AR 12712 observed with both Hi-C 2.1 and AIA 171. From these five regions, 14 cross-sectional slices are taken that intersect perpendicular to observed coronal strands. Four of these slices are taken from a region of comparatively low emission (Section 3.1), and ten from four regions of much higher observed emission (Section 3.2). In Section 3.3, the widths of the coronal strands are then determined and compared to previous high-resolution findings; the conclusions arising from these results are discussed in Section 4.

2. Hi-C 2.1 Observations and Data Analysis Techniques

On 2018 May 29 at 18:54 UT, Hi-C was successfully relaunched from the White Sands Missile Range, NM, USA, capturing high-resolution data (2k × 2k pixels, 4farcm× 4farcm4 field of view) of target active region AR 12712. This was the third flight for the Hi-C instrument; the second flight was nominal but the instrument suffered from a shutter malfunction such that no data were captured. For this reason, the mission reported upon here is named Hi-C 2.1. Unlike the first mission that captured EUV images in the narrowband 19.3 nm channel (dominated by Fe xii emission ≈1.5 MK), this mission focuses on EUV emission of wavelength 17.2 nm (dominated by Fe ix emission ≈0.8 MK), which has a similar temperature response to the AIA 171 passband. Hi-C 2.1 has a plate scale of 0farcs129, and captured 78 images with a 2 s exposure time and a 4.4 s cadence between 18:56 and 19:02 UT. During the Hi-C 2.1 flight, the instrument experienced a pointing instability that resulted in periodic jitter in the data set. This jitter caused motion blur and lower spatial resolution in approximately half of the data captured. Furthermore, the data were further affected by the shadow of the mesh in the focal plane, reducing the intensity behind the mesh by up to ≈35%. Full details on the Hi-C 2.1 instrument can be found in Rachmeler et al. (2019).

The goal of the analysis outlined here is (i) to determine from visual inspection a possible range of the structure observed in the Hi-C 2.1 images and (ii) to measure the FWHM of these detected strands. This work samples subsections of the Hi-C 2.1 field of view (FOV), for which the data are time-averaged over a period of ≈60 s for both AIA and Hi-C 2.1, taking care to avoid the Hi-C 2.1 exposures impacted by the aforementioned jitter. This helps to improve the signal-to-noise ratio, particularly where the emission is low. Figure 1 shows the five regions from which 14 cross-sectional slices are taken. Their selection was predicated upon choosing locations where there is possible evidence of substructure or stranding within the loops, while taking care to avoid areas in the Hi-C 2.1 FOV where a shadow of the mesh is clearly seen.

Figure 1.

Figure 1. Left: full disk image captured by AIA 171. The dashed white lines indicate the target active region, AR 12712. Middle: image for AIA; right, image for Hi-C 2.1. The images have been averaged over the course of ≈60 s and sharpened using MGN. The middle panel indicates the regions studied in this paper. The low-emission loops (red), large loops bundle (green), two open fan regions (blue), and central loops bundle (black) are shown in more detail in Figures 48.

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To assist in visualizing the finest structures in the Hi-C 2.1 data, we employ an image processing technique. EUV images of the corona span a wide range of features and temperatures, from cooler, low-emission coronal holes, quiet Sun, and filament channels, through to bright, hotter active regions. To account for the dominance of the bright features and reveal low-emission structures often hidden in the data, Morgan & Druckmüller (2014) developed the multi-scale Gaussian normalization (MGN) technique for image processing. The method is based on localized normalization over a range of spatial scales, and thus MGN can reveal the fine detail in the corona and structures in off-limb regions without introducing artifacts or bias. The technique is commonly used in detection of coronal mass ejections (CMEs) and stealth CMEs (Alzate & Morgan 2017; Hutton & Morgan 2017; Long et al. 2018), but is also used in coronal loop studies (Chitta et al. 2017; Long et al. 2017).

Due to the way MGN enhances peaks in low-emission plasma, and depresses them in high-emission plasma, the technique is only employed in this work to improve the visual inspection of the AIA and Hi-C 2.1 data. If the FWHM calculations undertaken in Section 3 are done on MGN-processed data, they will lead to artificially narrowed (broadened) strands in low- (high-)emission plasma. Adapting the method outlined by Pant et al. (2015) in relation to the first Hi-C mission, two low-frequency passband filters are applied to both the original and MGN-sharpened Hi-C 2.1 data sets to reduce the granular noise present.

In order to determine the widths of the structures, we extract the Hi-C 2.1 and AIA intensity along slices inside each subregion; an example intensity profile is shown in the left panel of Figure 2. To further increase the signal-to-noise ratio, the slices in Hi-C 2.1 and AIA are taken to be 3 pixels wide; the intensity is then averaged over these pixels. The slices are taken perpendicular to the strand cross section in order to obtain accurate measurements of the strand widths. The slice locations and averaged intensities in AIA and Hi-C 2.1 are given in Figures 48 in the first and second columns, respectively. After finding the average intensity along each slice, the global trend is removed by finding all the local minima of a slice (shown in Figure 2 as red asterisks), and interpolating through these values. The resulting trend is then subtracted from the intensity profile of the slice, leaving behind the variations, i.e., the coronal strands, seen in the right panel of Figure 2 and the third columns of Figures 48. The base locations of the isolated coronal strands are determined as the inflection points, and the maximum value between the two inflection points is taken as the maximum of each strand. From these two values, the half-maximum value is determined and their locations are used to determine the FWHM of each structure analyzed (orange dashed lines in Figure 2). These FWHM values are used as a possible determination of the coronal strand widths, which are then compared to previous high-resolution studies.

Figure 2.

Figure 2. A subsection of Hi-C 2.1 intensity slice 10 (left) is shown here to demonstrate the process of background removal from the cross-sectional slices analyzed. The red asterisks denote the locations through which we interpolate to obtain the global background. Right: the same Hi-C 2.1 intensity profile with the global background having been deducted. The blue and green asterisks denote the base and maximum values used to determine the height of the peak. The half-maximum is then determined as the midpoint between these two values and is used to determine the FWHM (dashed orange lines).

Standard image High-resolution image

The uncertainty in the intensity for the cross-sectional slices is determined by ${\rm{\Delta }}I=\sqrt{I}$. If the slice under consideration is from a region where the intensity is low, ΔI will correspond to a larger proportion of the intensity than for a slice from a region of greater intensity. In some instances, such as slice 10 (Figure 6), the magnitude of ΔI appears to increase once the background has been subtracted (variation slice 10). This is merely a consequence of the background emission being large relative to the local intensity of the coronal strands itself. Renormalizing the background-subtracted slices has the effect of focusing in on the structures themselves, which thus means that ΔI will appear larger.

3. Results

In this study cross-sectional profiles are taken from structures observed within five regions, whose positions in the AIA and Hi-C 2.1 FOV are indicated in Figure 1. Table 1 indicates the average emission for all five regions investigated during the ≈60 s for which the data are time-averaged. As is seen in Table 1, the average emission of Region A is at least an order of magnitude lower than that of other locations investigated within AR 12712. For this reason, the study is split into two parts in what we term in this paper as low-emission loops (Region A in Figure 1) and four high-emission loop regions (Regions B–E in Figure 1). The low-emission loops are shown in more detail in Figure 4, while the high-emission regions include a selection of loops: large loops (Figure 5), open fan loop regions (Figures 6 and 7), and some small loops close to the center of the active region (Figure 8).

Table 1.  Average Emission for All Pixels in the Regions Studied over the ≈60 s Time-averaged Data

Region in Figure 1 Loop Type Mean Emission Hi-C 2.1 Mean Emission AIA
    (DN/pixel) (DN/pixel)
A Low-emission loops 1229.13 211.550
B Large loops bundle 44892.5 3792.84
C Northern open fan loops 79550.3 6939.30
D Southern open fan loops 55688.6 4983.92
E Central loops bundle 46270.3 3720.91

Download table as:  ASCIITypeset image

Figure 3 shows the the Helioseismic and Magnetic Imager (HMI) line-of-sight (LOS) magnetic field for the Hi-C 2.1 FOV and the surrounding area. The snapshot shown here is taken at 18:56:15 UT, which corresponds to the ≈60 s period under examination with Hi-C 2.1 and AIA. From this it can be seen that AR 12712 resides above a diffuse bipolar region.

Figure 3.

Figure 3. HMI line-of-sight magnetic field for the Hi-C 2.1 FOV (white) and the surrounding area. The five regions (A–E) examined in the study are indicated in the same manner as Figure 1.

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The closed magnetic loops under investigation in regions B and E very clearly have their footpoints rooted in the areas of opposite polarity, likely crossing over the active region's polarity inversion line. The open fan loops observed in regions C and D originate from areas of opposite polarity. The low-emission strands observed in region A have one footpoint in the area of positive polarity but their negative-polarity footpoint lies outside the Hi-C 2.1 FOV. However, these low-emission strands are still an integral part of the overall active region itself.

The strands in region A are low-density, and subsequently low-emission. However, their location and ideal viewing angle place them away from the core of the active region, so these strands can be observed in a more isolated manner, helping us to determine their widths. The coronal magnetic field is often considered to be force-free in 3D simulations (Aschwanden 2019 and references therein), which implies that current density scales with the magnetic field (e.g., Figure 1 in Gudiksen & Nordlund 2002). One may expect the heating to be greater where current density is larger, and subsequently the emission to be higher. For these reasons, the study is separated into low-emission (Section 3.1) and high-emission (Section 3.2) regions.

3.1. Low-emission Loops

Given the way that MGN normalizes a range of emission, Figure 4 indicates visually the fine-scale structure that is present even in regions that may initially appear to be beneath the detection threshold. The top left panel shows the MGN-sharpened AIA time-averaged data, and the bottom left panel shows the corresponding MGN-sharpened Hi-C 2.1 image. From these two images, it can be seen that AIA does not have the resolution to differentiate some of the lower density, low-emission strands above the background corona and instrumental noise. Hi-C 2.1, on the other hand, performs much better, with several low-density strands being observably distinguishable.

Figure 4.

Figure 4. The two images in the left column indicate the location of the low-emission loops for AIA (top) and Hi-C 2.1 (bottom). The intensity slices are numbered 1 through 4, indicating the cross sections under consideration. The middle column shows the time-averaged plots of intensity along the cross-sectional slices for AIA (red) and Hi-C 2.1 (black). Here, slice position from left to right corresponds to south-to-north orientation in the images. The right column shows the detrended, time-averaged variations of each slice, i.e., the slices with the global trends having been subtracted. The error bars indicate the uncertainty in the intensity, which is defined as ${\rm{\Delta }}I=\sqrt{I}$.

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Four data slices are taken across Region A (numbered 1–4 in Figure 4) and the normalized emission intensity along each slice is compared for Hi-C 2.1 and AIA. Each intensity profile is plotted from south-to-north. Slices 1 and 2 show good agreement between Hi-C 2.1 and AIA, particularly with the broader structure centered around 9''. However, there are signs of the structure consisting of more than a single strand in Hi-C 2.1 due to the irregular shape. South of this in slice 2 there is a single strand in the AIA data (2''–6farcs5), but in Hi-C 2.1 there is evidence of three coronal strands, which trace the same envelope resolved by AIA. These Hi-C 2.1 structures have FWHM between 345 and 396 km, which is less than the width of a single AIA pixel.

The difference between the two instruments becomes more apparent in slices 3 and 4. In the MGN-sharpened images, it can be seen in the southernmost part of the slices that there are three distinct strands for Hi-C 2.1 and one to two strands in the corresponding AIA envelope. However, in the time-averaged slices for the non-MGN-processed Hi-C 2.1 data, only two peaks can be seen in slice 3 (between 5'' and 12'') and one peak in slice 4 (3''–11''). This arises because of the way in which MGN normalizes and enhances over a range of spatial scales and thus cannot be employed for direct data analysis in this study.

Further north of this large envelope (12''–25''), it can be seen that there is plasma detected by AIA, but this is noisy with no structure being resolved. This can be seen in the time-averaged slices because the normalized intensity value is between ≈0.85 and 0.95 but no individual peaks can be identified that are above the error bars. For Hi-C 2.1, however, there are multiple strands resolved in this region, with five strands resolved between 14'' and 25'' in slice 3, and eight strands between 11'' and 24'' in slice 4.

3.2. High-emission Measure Loops

In this subsection results from investigations of 10 cross-sectional slices in the high-emission loop regions (B–E in Figure 1) are presented in the same manner as the low-emission loops discussed in Section 3.1. Again, the normalized intensity profiles are plotted but left to right orientation now corresponds to west-to-east in the respective AIA and Hi-C 2.1 images (Figures 58).

Figure 5.

Figure 5. The same layout and approach as in Figure 4 but for the large loops bundle in the southwest quadrant of the Hi-C 2.1 FOV. Note: slice position left to right in the intensity plots corresponds to west-to-east orientation in the images. The error bars indicate the uncertainty in the intensity, which is defined as ${\rm{\Delta }}I=\sqrt{I}$.

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The cross-sectional slices typically show similar intensity profiles for Hi-C 2.1 and AIA, with many structures being nearly identical. In particular, slices 7 (Figure 5), 8, 10 (Figure 6), and 11 (Figure 7) display strikingly similar overall profiles in Hi-C 2.1 and AIA. The only appreciable differences seen in slices 7 (7''–12''), 8 (17''–23''), and 10 (6''–10'') occur where single AIA strands correspond to two Hi-C 2.1 strands, which have widths of 562 and 1146 km in slice 7, 1333 and 923 km in slice 8, and 985 and 556 km in slice 10, placing them approximately between one and three AIA pixel widths.

Figure 6.

Figure 6. The same layout and approach as in Figure 4 but for the north open fan loops in the northwest quadrant of Hi-C 2.1 FOV. Note: slice position left to right in the intensity plots corresponds to west-to-east orientation in the images. The error bars indicate the uncertainty in the intensity, which is defined as ${\rm{\Delta }}I=\sqrt{I}$.

Standard image High-resolution image
Figure 7.

Figure 7. The same layout and approach as in Figure 4 but for the south open fan loops in the southeast quadrant of the Hi-C 2.1 FOV. Note: slice position left to right in the intensity plots corresponds to west-to-east orientation in the images. The error bars indicate the uncertainty in the intensity, which is defined as ${\rm{\Delta }}I=\sqrt{I}$.

Standard image High-resolution image

Similarly, there are also examples where although Hi-C 2.1 and AIA observe the same general structure, Hi-C 2.1 potentially resolves more coronal structures along the length of the cross sections, such as is seen in slices 5 and 6 (Figure 5), and slice 13 (Figure 8). In these three slices there is reduced commonality between the two instruments because the variations are increased compared to the nearly identical cross sections seen in slices 7, 8, 10, and 11. Focusing on slice 5, the time-averaged intensity plots of both instruments appear to show agreement; however, the corresponding detrended profile (variation plot 5 in Figure 5) reveals important differences. This can most notably be seen with the AIA structure centred at 5'' spanning between two Hi-C 2.1 strands. Further along slice 5, the AIA structure is double-peaked, with the corresponding emission coming from two distinct structures in Hi-C 2.1. Other examples can be seen in slices 6 (0''–19'') and 13 (1farcs5–4'' and 7''–13'').

Figure 8.

Figure 8. The same layout and approach as in Figure 4 but for the central loops bundle between the central moss and low-emission loops. Note: slice position left to right in the intensity plots corresponds to south-to-north orientation in the images. The error bars indicate the uncertainty in the intensity, which is defined as ${\rm{\Delta }}I=\sqrt{I}$.

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It is slices 9, 12, and 14 that the difference in resolution, and subsequently resolving power of the two instruments is most notable for the high-emission regions. In the range of slice position 0''–8'' in slice 9 (Figure 6) there is a single, large structure in AIA, which can be seen as two peaks in the time-averaged Hi-C 2.1 data. This double peak is evident in the corresponding MGN Hi-C 2.1 image, while in the MGN AIA image the structure still appears monolithic.

Closer inspection of the two Hi-C 2.1 structures (0''–7'') in the variation plot reveals that the "monolithic" AIA structure could actually be composed of four strands. This is because, while the detrended profiles of the Hi-C 2.1 structures are large, the peaks of the two structures are actually composed of two small peaks, which are fully resolved and above the error bars.

The next AIA structure in slice 9 also appears as a broad, mostly unresolved single feature detected at position 19''. However, in the corresponding Hi-C 2.1 data there are two strands. Similarly, for the rest of the slice, Hi-C 2.1 detects two more strands, both indicating signs of possible substructure with faint double peaks like the two aforementioned Hi-C 2.1 structures (0''–7''). This highlights that there is evidence for further substructuring beyond anything that Hi-C 2.1 can observe.

In slice 12 (Figure 7) we see one of the clearest examples where the increased resolving power of Hi-C 2.1 reveals strands that AIA does not distinguish. The two large AIA features in the ranges 1''–5'' and 5''–9'' each correspond to three Hi-C 2.1 strands, which have a mean width of 579 km. In Figure 8, slice 14 samples the cross section of two strands that are relatively isolated against the underlying moss region. The southernmost strand (≈0''–1farcs6) shows good agreement between Hi-C 2.1 and AIA in the variation plot, though again there is a non-smooth, irregular distribution in the Hi-C 2.1 data hinting at unresolved coronal strands. The northernmost strand (≈1farcs9–3farcs7) is well defined in Hi-C 2.1 with no obvious signs of substructure. However, in AIA there is no structure/peak at this location. The corresponding MGN-sharpened AIA image reveals that the strand fades in and out of detection along its length, indicating that this strand is at the detection threshold of AIA. This could mean that either this is a low-emission strand, or the strand has a very narrow or precise temperature that is very close to the peak emission temperature of Hi-C 2.1.

3.3. Strand Widths

A total of 25 and 49 strand widths are measured in the low-emission and high-emission regions, respectively. The Appendix contains two tables that index the widths and locations of all the strands measured by Hi-C 2.1 and AIA for the low-emission (Table 2) and high-emission (Table 3) regions.

However, as can be seen in slices 3 and 12, some of the structures are double-peaked. Consequently, these either result from the presence of strands beneath the resolving power of Hi-C 2.1 or are due to other coronal plasma somewhere else along the integrated line of sight due to the plasma being optically thin. Measuring the widths of these structures could lead to an artificially broadened distribution. Subsequently, analysis is undertaken with these double-peaked structures discarded from this survey, hence leaving 19 low-emission strands and 30 high-emission strands for width analysis. Thus, the widths are collated into plots of occurrence frequency in Figure 9 for the low-emission strands and in Figure 10 for the high-emission strands.

Figure 9.

Figure 9. This figure collates the strand widths measured for the low-emission region. The top two panels display plots of occurrence frequency of strand width against number of strands observed for all the strands measured using Hi-C 2.1 and AIA. The bottom two panels show the same plots of occurrence frequency but now for 19 single-peak strands in Hi-C 2.1 and 10 single-peak strands in AIA. The Hi-C 2.1 widths are shown in 125 km bins, whereas the AIA bin width is 250 km.

Standard image High-resolution image
Figure 10.

Figure 10. This figure collates the strand widths measured for the high-emission regions. The top two panels display plots of occurrence frequency of strand width against number of strands observed for all the strands measured using Hi-C 2.1 and AIA. The bottom two panels show the same plots of occurrence frequency but now for 30 single-peak strands in Hi-C 2.1 and 25 single-peak strands in AIA. The Hi-C 2.1 widths are shown in 125 km bins, whereas the AIA bin width is 250 km.

Standard image High-resolution image

The Hi-C 2.1 plot of occurrence frequency for the low-emission strand widths (Figure 9) reveals that there are low-density, low-emission strands at both ends of the spatial scale, with structures as small as ≈200 km and as large as 1700–1950 km. However, these broader structures have irregular intensity profiles (as mentioned in Section 3.1). Consequently, when only single-peaked structures are considered, the broader strands are between 825 and 950 km, which is narrower than the most likely strand width measured with AIA (950–1200 km). For Hi-C 2.1, the most likely strand width of the low-emission structures is 325–450 km, placing the structures at approximately the same width as an AIA pixel or smaller.

Figure 10 shows a similar distribution of strand widths for the four high-emission regions as is seen with the low-emission region. Again, narrow strands ≈200 km wide are detected by Hi-C 2.1 though these are not as prevalent as in the low-emission region despite a larger sample of structures being investigated. Additionally, broader strands with widths >1000 km are observed in the high-emission regions, with one strand in slice 11 (≈19''–24farcs6) exceeding a width of 2000 km. The most likely strand width for single-peaked structures in the four high-emission regions is between 450 and 575 km. Considering that the smallest structure partially resolved by AIA (466 km) is larger than the average low-emission strand width resolved by Hi-C 2.1 (≈388 km), it could be argued that these results, alongside those from the maiden flight of Hi-C, provide compelling evidence for satellite-borne instrumentation with the resolving power of at least Hi-C.

For AIA, the most likely strand widths of the low-emission and high-emission regions are the same (≈1075 km), but for Hi-C 2.1 the low-emission strands are approximately 125 km narrower than those resolved in the high-emission region (≈388 versus ≈513 km). It is worth noting that there is a greater proportion of the low-emission strands than high-emission strands with widths between 200 and 325 km. Conversely, the high-emission strands often exhibit widths ⪆1000 km, agreeing with results from Peter et al. (2013), while the low-emission strand widths do not exceed 950 km in this study.

4. Concluding Remarks

Continuing on from the success of Hi-C, Hi-C 2.1 reveals structures throughout and around its targeted active region (AR 12712) in the 17.2 nm line that cannot be resolved by SDO/AIA. The work outlined here investigates five regions from the Hi-C 2.1 FOV, one region of which could be considered low-emission and the other four of significantly increased emission (Figure 1).

In regard to Region A, although it could be argued that there are hints of faint structures that could be observed in the AIA FOV, it is found that with Hi-C 2.1's superior resolving power, this region is in fact filled with numerous low-emission, and hence low-density strands. In AIA, these strands often appear as granular noise. A contributing factor to this is that these low-emission strands are observed by Hi-C 2.1 to be of only ≈388 km in width, below the scale of a single AIA pixel.

In contrast, Regions B–E have higher emission structures with an average Hi-C 2.1 strand width of ≈513 km, placing them in line with previous width measurements made using Hi-C (Brooks et al. 2013; Aschwanden & Peter 2017). As discussed in Peter et al. (2013) with regard to miniature loops, the Hi-C 2.1 data reveal strand widths as small as 200 km in both the low-emission and high-emission regions, though they appear to be more numerous in the low-emission area of the active region.

An intriguing result is outlined in the analysis of slice 14, which samples the cross section of the closed active-region loops near the center of the Hi-C 2.1 FOV. In the MGN-sharpened AIA image (Figure 8), the northernmost strand sampled in slice 14 appears to fade in and out of AIA detection along its length. This suggests that the plasma contained within this structure is at the sensitivity limit of AIA, even when advanced image processing techniques such as MGN are employed. Either this is a low-emission strand among the high-emission structures, or it may simply be due to the fact that AIA and Hi-C 2.1 observe plasma at slightly different temperatures (17.1 and 17.2 nm emission).

The evidence for low-emission strands, which are very difficult to observe with AIA but much better resolved and with their width better determined by Hi-C 2.1, strongly indicates that plasma threads with low-density but coronal-temperature material are prevalent throughout the corona. This may be a strong indicator of previously unresolved but background-heated corona that Hi-C 2.1 is beginning to provide evidence for. However, even with the enhanced spatial resolution of Hi-C 2.1, it still appears that there are structures that could not be fully resolved. Although this could be due to projection effects of the optically thin plasma viewed along its LOS, another possible scenario is that there are coronal strands with structural widths below even the resolving power of Hi-C 2.1.

Slices 9 and 12 are good examples of this but there are hints of substructure above the observational error throughout all the slices examined. Thus, it may be possible for an instrument of greater resolving power to discriminate between these features. Note that by combining both fast Fourier transform methods and Gaussian width analysis, Rachmeler et al. (2019) conclude that the Hi-C 2.1 resolution is between 0farcs3 and 0farcs47 (≈220–340 km) in images that are not affected by motion blur. The most likely widths obtained for the low-emission strands (≈388 km) are above the resolution limit of Hi-C 2.1, indicating that at this increased spatial resolution we may be beginning to have the opportunity to resolve a fundamental width of individual coronal strands. This result agrees with the results from Aschwanden & Peter (2017), though we note that there is accumulating evidence of strands with widths beneath the Hi-C 2.1 resolution.

Additionally, it may be argued that spatial structuring is only one part of the data required to address this question of basic plasma stranding because the spread of observed temperature of these features is also critical. If the 17.2 nm Hi-C 2.1 structures that are observed to be below the AIA resolution limit could also be observed in other passbands with similar spatial resolution to Hi-C 2.1, and those observations then resulted in a broad temperature distribution of many strand-like features, then this could be strong evidence for multi-thermal, many-stranded models being the best way to tackle coronal heating.

Future work will further examine the double-peaked structures by fitting appropriate Gaussian profiles in order to estimate the widths of the possible sub-resolution strands, as well as consider the examination of the extrapolated magnetic field structure associated with low-emission strands alongside a comparison of the Hi-C 2.1 observations with modeling of specific active regions (Warnecke & Peter 2019).

We acknowledge the High-Resolution Coronal Imager (Hi-C 2.1) instrument team for making the second re-flight data available under NASA Heliophysics Technology and Instrument Development for Science (HTIDS) Low Cost Access to Space (LCAS) program (proposal HTIDS17_2-0033). MSFC/NASA led the mission with partners including the Smithsonian Astrophysical Observatory, the University of Central Lancashire, and Lockheed Martin Solar and Astrophysics Laboratory. Hi-C 2.1 was launched out of the White Sands Missile Range on 2018 May 29. S.K.T. gratefully acknowledges support by NASA contracts NNG09FA40C (IRIS) and NNM07AA01C (Hinode). The work of D.H.B. was performed under contract to the Naval Research Laboratory and funded by the NASA Hinode program.

Appendix

In this appendix we present Tables 2 and 3. These show all the strands where FWHM calculations were possible. The widths shown in bold with an asterisk denote strands that display obvious signs of sub-resolution and/or overlapping strands, and are thus omitted from final statistical analysis on the widths.

Table 2.  FWHM for the Investigated Low-emission Loops

Hi-C 2.1 AIA 171 Å
Slice # Start Position (arcsec) End Position (arcsec) FWHM (km) Slice # Start Position (arcsec) End Position (arcsec) FWHM (km)
1 0.000 1.968 697.5        
1 1.968 3.150 473.6        
1 4.987 5.906 381.2 1 4.200 13.20 2383.8*
1 5.906 11.28 1819.4*        
1 12.20 13.51 409.8        
2 0.000 1.050 226.6        
2 1.050 2.625 345.2 2 1.800 6.600 1373.4*
2 2.625 3.937 359.4        
2 4.200 5.643 395.5 2 6.600 12.60 2041.6
2 6.037 11.81 1859.0*        
3 1.806 4.644 733.9 3 0.600 4.200 838.7
3 5.031 7.224 822.0* 3 5.400 7.800 853.2
3 7.224 10.57 928.9 3 7.800 10.80 1062.1
3 14.06 15.73 552.0 3 15.00 17.40 642.6
3 16.12 18.31 590.9 3 17.40 21.00 1130.1
3 18.83 21.02 972.0* 3 21.00 23.40 925.7
3 21.02 22.96 620.5*        
4 11.61 12.25 215.7 4 4.200 6.600 951.2
4 12.65 13.67 664.6        
4 14.06 14.96 318.0 4 6.600 10.80 1829.0
4 14.96 16.12 527.4        
4 16.12 16.89 216.8 4 13.20 21.00 2701.2
4 17.93 19.35 466.7        
4 19.73 21.67 863.7 4 21.60 24.60 959.9
4 21.67 23.09 717.4*        

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Table 3.  FWHM for the Investigated High-emission Loops

Hi-C 2.1 AIA 171 Å
Slice # Start Position (arcsec) End Position (arcsec) FWHM (km) Slice # Start Position (arcsec) End Position (arcsec) FWHM (km)
5 0.000 1.712 528.5        
5 1.913 5.640 1346.6* 5 3.748 6.559 1547.6
5 9.267 11.88 1190.5* 5 8.901 12.18 1513.0
5 11.88 14.20 871.2 5 12.18 14.52 1137.4
5 14.40 15.31 202.2        
6 4.515 8.256 1046.0 6 0.600 2.400 895.2
6 8.256 9.417 355.8 6 2.400 7.800 1781.3*
6 9.417 13.15 1047.7 6 7.800 16.20 2840.0
6 30.18 32.89 1107.1 6 16.20 18.60 893.8
7 1.783 7.220 2304.5* 7 1.975 7.506 2279.2*
7 7.220 8.749 562.0 7 7.506 13.03 1577.4
7 8.749 11.38 1146.1 7 13.03 19.75 1722.2*
7 13.25 19.19 1862.4* 7 19.75 22.91 1135.9
7 19.53 22.42 1028.8        
8 1.806 4.386 810.6 8 1.200 4.800 819.5
8 4.386 10.96 2453.3* 8 4.800 10.20 2550.0*
8 10.96 15.35 1775.4 8 10.20 15.60 1571.2*
8 16.51 20.51 1333.7 8 16.80 22.80 1782.1
8 20.51 22.70 922.7* 8 22.80 24.60 708.2
8 24.76 27.47 676.9        
9 0.000 4.164 1509.6*        
9 4.164 7.192 1180.6* 9 0.000 7.630 3241.7
9 7.823 11.60 1392.5* 9 7.630 10.56 1083.7
9 11.60 15.52 1145.8* 9 11.73 13.49 736.6
9 17.41 19.18 646.0* 9 15.26 17.02 536.6
9 19.18 21.07 750.7 9 17.02 21.71 1374.2
10 0.369 3.447 1071.2* 10 0.000 3.436 1306.2
10 3.447 6.156 975.4 10 3.436 6.299 1143.2
10 6.156 8.618 984.9 10 6.299 9.735 969.1*
10 8.618 10.09 556.3        
11 0.258 4.515 1622.4 11 0.000 4.800 1939.5
11 4.515 9.417 1718.9* 11 4.800 10.20 1504.7
11 18.96 24.63 2069.9 11 18.60 27.00 3116.1
12 0.121 1.274 387.2        
12 1.274 3.096 830.9* 12 0.000 1.129 532.8
12 3.096 4.128 346.4        
12 4.128 5.524 571.9 12 1.129 5.364 1485.1*
12 5.524 6.799 451.6        
12 6.799 8.316 534.0 12 5.364 9.317 1633.6*
12 8.316 9.834 738.7*        
13 0.081 2.042 560.5* 13 0.000 1.159 589.8
13 2.042 3.185 382.2        
13 3.349 4.084 263.3 13 4.179 6.838 977.6
13 4.084 6.371 795.4*        
13 7.270 9.149 582.1 13 7.598 9.498 466.6
13 9.149 10.04 400.0        
13 10.04 11.51 574.9 13 9.498 11.77 967.4
14 0.000 1.733 685.2* 14 0.000 2.121 571.6
14 1.915 3.739 478.4        

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