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IN et al.
1
TEST OF THE ITER-LIKE RMP CONFIGURATIONS
FOR ELM-CRASH-SUPPRESSION ON KSTAR
Y. IN
National Fusion Research Institute
Daejeon, Republic of Korea
Ulsan National Institute of Science and Technology
Ulsan, Korea
Email: [email protected]
Y.M. JEON, H.H. LEE, K. KIM, G.Y. PARK, and 3D Physics Task Force in KSTAR
National Fusion Research Institute
Daejeon, Republic of Korea
H. PARK, and M.W. KIM
National Fusion Research Institute
Daejeon, Republic of Korea
Ulsan National Institute of Science and Technology
Ulsan, Korea
J.K. PARK
Princeton Plasma Physics Laboratory
Princeton, Unites States of America
A. LOARTE
ITER organization
St. Paul Lez Durance, France
and
J.W. AHN
Oak Ridge National Laboratory
Oak Ridge, Unites States of America
Abstract
KSTAR has demonstrated divertor heat flux broadening during edge-localized-mode (ELM)-crash-suppression using
ITER-like 3-row resonant magnetic perturbation (RMP) for the first time. To address a couple of critical issues in ITER
RMP, robust ELM-crash-suppression methodology has been explored at low q95 and established in KSTAR using low-n
RMPs. Taking full advantage of the ITER-like 3-row in-vessel control coils (IVCC) in KSTAR, a set of intentionally
misaligned RMP configurations (IMC) was tested to investigate whether or not IMC could be compatible with ELM-crash-
suppression, while minimizing electromagnetic loads on RMP coils. As a result, the ITER-like 3-row IMCs were found not
only to have been compatible with the ELM-crash-suppression, but also to have broadened the heat flux in the vicinity of the
outer strike point on divertor. In comparison, the 2-row RMPs have rarely affected the near scrape-off-layer (SOL) heat flux
despite slightly broadened profile change in the far-SOL. Since the divertor heat flux broadening reflects the dispersal of the
peaked near-SOL heat flux, the experimental outcome is quite favorable to the ITER choice of 3-rows, instead of 2-rows.
Nonetheless, since the IMC-driven broadening observed in the attached plasmas in KSTAR might appear substantially
different in the partially detached plasmas in ITER, additional investigation has been conducted to see if RMP-driven, ELM-
crash-suppression could be compatible with detached plasmas. Although no detached plasmas have been identified with
ELM-crash-suppression yet, significantly reduced divertor heat flux was confirmed in high density, ELM-crash-suppressed
plasmas at q95=3.8 using n=2 RMPs. These new findings elevate the confidence level about the ITER RMP system, while the
remaining uncertainties need to be further clarified using the 3-row IVCCs in KSTAR. As long as mode-locking percussion
is minimized along with a quick recovery of wall conditions, the access to the targeted q95 (~ 3) for ITER is foreseen to be
feasible in KSTAR.
1. INTRODUCTION
The success of ITER is of paramount importance not only to enhance the scientific understanding of nuclear
fusion, but also to evaluate the technological feasibility of nuclear fusion reactor [1]. Considering that high
confinement mode (H-mode) operation in ITER is expected to be accompanied by edge-localized-modes (ELM),
EX7-1
a robust and reliable control to either suppress or mitigate
ELMs is a must, not an option, in that the ELM-driven
particle and heat fluxes could endanger the integrity of
the divertor and plasma facing components [2]. One of
the critical issues in the planned ITER resonant magnetic
perturbation (RMP) system require the divertor heat flux
to be sustained below the critical thresholds of material
safety; ~ 10MW/m2 (in steady state), except for ~20
MW/m2 (transiently)[2]. To meet the criteria, several heat
load dissipation methods can be considered, including
rotating RMP [3]. However, due to the concern about
material fatigue related to time-varying electromagnetic
(EM) loads on coils [2, 3], intentionally misaligned
configurations (IMC) have been proposed to not only
spread the divertor heat fluxes, but also alleviate the EM
loads on coils. Unlike many devices (typically equipped
with 2-row RMPs of Upper/Lower coils), the planned
ITER RMP system is composed of 3-row RMP coils. In
that regard, the KSTAR provides an ideal environment
for ITER RMP study, in that robust RMP-driven, ELM-
crash-suppression has been routinely accessible using
ITER-like 3-row in-vessel control coils (IVCC) [4].
Indeed, over the last couple of years, we have established
a robust methodology to fully suppress ELM-crashes
using low-n (i.e. n=1 or 2) RMPs. To address the ITER
relevant ELM control, a systematic exploration of various
RMP configurations at lower q95 plasmas led us to
accomplish RMP-driven, ELM suppression down to q95 =
3.3[5]. Here, n and q95 refer to the toroidal mode number
and edge safety factor at the 95 % normalized flux surface
respectively. As expected, such low q95 plasmas were
found to be much more vulnerable to mode-locking,
which might have changed the wall conditions substantially. Thus, as long as mode-lockings are avoided and a
quick recovery of the wall conditioning (e.g. cryo-pumping or divertor gas-puffing) is secured, the access to the
targeted q95 (~ 3) for ITER is foreseen to be feasible in KSTAR in the near future. Figure 1 shows one of the
nearly stationery ELM-crash-suppressions using n=1 RMP at q95 = 5, whose sustainment of ~30 sec is
comparable to the deuterium fuel wall saturation time in KSTAR [4]. While the ITER-RMP system has been
designed for n=3 or 4 under the ITER baseline scenario (IBS) at q95 ~ 3 [6], the test of ITER-like RMP
configurations has been conducted at various q95 using the low-n RMPs. Specifically, taking full advantage of 3-
row IVCC in KSTAR, a series of intentionally misaligned RMP configurations have been investigated for ELM-
crash-suppression and the relevant divertor heat flux distribution. As a result, we have not only demonstrated the
compatibility of the IMC-driven, ELM-crash-suppression, but also identified a few promising IMC
configurations that could be more effectively used to disperse the divertor heat fluxes in a wider area.
In Section 2, the ITER-like RMP configurations, along with the experimental setup, will be briefly introduced.
In Section 3, the divertor heat fluxes under various IMC-driven, ELM-crash-suppressions are summarized,
while an emphasis is given to the difference of the divertor heat flux broadening between 3-row and 2-row RMP
configurations. In Section 4, a simple linear modelling has been proposed and evaluated with field-line-tracing
calculations, which appears partly consistent with the experimental observations. In Section 5, the progress
about the compatibility study of ELM-crash-suppression with detached plasmas is reported. In Section 6, the
remaining physics tasks and prospects are discussed, along with a short summary.
2. ITER-LIKE RMP CONFIGURATIONS AND EXPERIMENTAL SETUP
To minimize the time-varying EM loads on RMP coils, 3 types of 3-row n=1 RMP configurations have been
explored, while a 2-row n=1 RMP (Upper/Lower rows) configuration without mid-RMP has been compared, as
schematically shown in Figure 2. All of the 3-row intentionally misaligned configurations (IMC) are compared
with the reference configuration of 90° phasing of n=1 RMP. Here, the phasing refers to the toroidal phase
difference between adjacent rows. In KSTAR, such 90° phasing (default) of n=1 RMP has been frequently used
and confirmed effective in suppressing ELM-crashes, as illustrated in Figure 1.
Fig. 1
IN et al.
3
Fig. 2
°
To diagnose the divertor heat fluxes during
RMP-driven, ELM-crash-suppression, a
toroidally rotating n=1 RMP has been applied,
while a high-resolution infrared (IR) camera up
to 9 kHz sampling(~100 s) is utilized [7].
According to a recent study of Type I ELMs, the
duration of ELMy burst of ~400 s (with a peak
of up to ~50 MW/m2 without RMPs) is longer
than a typical parallel connection time of ~200
s. Thus, a divertor heat flux striation pattern
associated with a slowly rotating RMP at 1 Hz
can be accurately probed by such a rotating
RMP, where its plasma response beyond
vacuum calculation needs to be separately
considered. As will be discussed in Section 4,
the measured divertor heat fluxes are compared with the field-line-tracing calculations [8].
3. DIVERTOR HEAT FLUXES DURING IMC-DRIVEN, ELM-CRASH-SUPPRESSION
First of all, all the attempted 3-row IMCs, as well as 2-row RMPs, are confirmed to be more or less compatible
with ELM-crash-suppression, although the allowable degree of misalignment from the reference phasings varies
subject to a type of 3-D configuration.
3.1. 3-row IMC-driven, ELM-crash-suppression and its divertor heat fluxes
Figure 3 shows one of the successful IMC-driven, ELM-crash-suppressions, whose toroidal phases between
rows move “toward” each other. Each phasing is sustained for 2 sec in static IMC, followed by a toroidally
rotating IMC for 1 sec, like a rigid body. As a
result, the IMC-driven, ELM-crash-suppression on
19212 has been fully sustained for both static and
rotating IMC until 10° of misalignment (up to 14
sec). Although the quality of ELM-crash-
suppression at the misalignment of 15° in static
IMC was not so perfect as those at the other
preceding misalignments, the ELM-crashes remain
suppressed in rotating IMC. Figure 4 shows the
measured divertor heat fluxes using the IR camera,
Fig. 4 Divertor heat flux measurement during the
intentionally misaligned 3-D configuration (IMC), as the
phasing between rows is moving “toward” each other by
the denoted amount in comparison with the reference
phasing of 90° (labelled as “0° ” here). Shown are
the time evolutions of the re-aligned divertor heat flux
from IR camera, whose raw signals are subject to radial
excursions within +/- a few millimeters.
Fig. 3 ELM-crash-suppression using intentionally misaligned 3-
D configuration (IMC). Shown are the time evolutions of (a)
two-color-interferometry (TCI) line-integrated average of plasma
density ne, (b) electron temperature Te,
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whose quantitative analysis would be feasible up to 17 sec. Note that the divertor heat flux measurements have
been realigned with the border line of private flux region, whose radial position differs from that of a raw IR
camera signal within +/- a few millimeters. Since such realignment leads to the most-stringent condition for
divertor material safety, it does not compromise any physics issues related to the divertor heat flux study, while
providing a more rigorous technical constraint on divertor heat flux distribution. The other 3-row IMCs (i.e.
‘distorted’ and ‘away’ phasings) were also confirmed to be compatible with the ELM-crash-suppression, as
reported elsewhere[5].
3.2. 2-row ELM-crash-suppression and its divertor heat fluxes
While 3-row RMP-
driven, ELM-crash-
suppression is
frequently used in
KSTAR, the 2-row
RMP-driven, ELM-
crash-suppression has
been newly
established for the first
time in 2017.
Primarily, an optimal
phasing for the
Upper/Lower rows of
RMP has been
predicted at -90 °
phasing, according to
the IPEC plasma
response
calculation[9]. As
schematically shown
in Figure 5, such
helical structure
appeared nearly
orthogonal to a typical
helical configuration
associated with 3-row
90 ° phasing in
vacuum. Nonetheless,
when the plasma response is considered for this 2-row RMPs of -90° phasing, the n=1 resonant components
turned out to be dominant, consistent with the experimental outcome. Hence, a systematic ‘adjustment’ from the
reference phasing of -90° has been similarly added to 2-row RMP, which would be exactly the same as a typical
n=1 phasing scan. Interestingly enough, all the supposedly ‘non-optimal’ phasings up to 20°, as denoted in each
configuration, were also found to be compatible with ELM-crash-suppression, as shown in Figure 5. The
corresponding divertor heat fluxes during static and rotating RMPs have been similarly re-aligned.
3.3. Divertor heat flux dispersal in 3-row IMC and 2-row RMPs
As aforementioned, the divertor heat flux dispersal with minimizing EM loads on coils has been investigated
using the rotating IMC and RMPs, which probe the toroidally non-uniform striation pattern on divertor, as
shown in Figs. 4 and 5 (b). While the misalignment increases in both 3-row IMC and 2-row RMP, the peaks of
divertor heat fluxes got reduced, as shown in Figure 6 (a) and (c) respectively. However, once the near-scrape-
off-layer (SOL) peaks are normalized, the divertor heat fluxes under 3-row IMCs have been broadened but
nothing similar appears in 2-row RMPs, as shown in Figure 6 (b) and (d). This reminds us of a similarly
contrasting observation of divertor heat fluxes between ELM-crash-suppression and ELM-crash-mitigation[5],
in which the divertor heat flux dispersal was observed only during ELM-crash-suppression, while nothing
similar appears during ELM-crash-mitigation. So far, when the IMC with “away” phasing is reinforced by the
global ‘kink-resonant’ influences, such broadening has been speculated to be readily available in a non-linear
plasma simulation [5]. On the other hand, the IMC with ‘toward’ phasing is essentially distanced from strong
Fig. 5 ELM-crash-suppression using 2-row (Upper and Lower RMPs only). Shown in (a) are
the time evolutions of (i) two-color-interferometry (TCI) line-integrated average of plasma
density ne, (ii) electron temperature Te,
the time evolution of the re-aligned divertor heat flux from IR camera and the
schematic of the 2-row IMC. Note that the reference phasing of the 2-row RMP is -90°
between Upper/Lower rows, which is equivalent to 270° in a longer path.
IN et al.
5
‘kink-resonance’ effect, so another non-linear coupling, possibly associated with ‘peeling’ dominance, may have
led to a similar broadening of divertor heat flux in this particular configuration.
Arguably, it is possible for the mid-row to have played a
bigger role than the other off-midplane rows in broadening
the heat fluxes. In particular, since the magnetic flux
delivered by the mid-row is roughly doubled than by the other
row in IVCC, such conjecture appears reasonable. In that
regard, even with 2-row RMPs, a similar divertor heat flux broadening might be accessible, as long as the mid-
row RMP is utilized. A follow-up experiment is scheduled to clarify whether or not the heat flux broadening is
exclusively attributable to 3-row IMCs in KSTAR.
4. DIVERTOR HEAT FLUX MODELLING AND FIELD-LINE-TRACING CALCULATTIONS
While each IMC of 3-rows, as well as 2-row RMP, has proven the compatibility with the ELM-crash-
suppression, the fundamental physics rationale responsible for divertor heat flux broadening at the near-SOL is
being investigated. To address such a rather complicated issue in a physically sound way, a simple modeling has
been established to correlate the divertor heat flux with edge temperature and density profiles.
4.1 Divertor heat flux specification for the 3-D field impact assessment on striation pattern
To evaluate the 2-D heat flux pattern in (Rdiv, ) at the outer divertor in KSTAR under the presence of the 3-D
field, a simple model is based on the following two assumptions:
First, for field lines at the divertor which are connected to the core plasma (of the unperturbed plasma without 3-
D fields), the heat flux at the divertor is determined by the plasma density and temperature at the corresponding
flux surface. It is assumed that there is direct connection between the core plasma and the divertor and that the
heat flows mostly along the field lines (i.e. no diffusion due to ergodic diffusion of fields lines). Second, for
field lines at the divertor which are connected to the SOL plasma the heat flux has the same dependency as the
Fig. 6 . Toroidally-averaged divertor heat fluxes and their
normalized shapes in 3-row and 2-row IMCs during ELM-crash-
suppression respectively. Shown on the left are the profiles of
toroidally-averaged divertor heat flux in each IMC, in comparison
with no RMP (black) and a typical rotating RMP with n = 1, +90°
phasing (red) with 3-rows in (a) and -90° phasing with 2-rows in
(c) respectively. On the right are the corresponding normalized
shapes of divertor heat flux at each configuration. Note that the
widths of A-A’ in (b) at the near SOL with 3-rows are broader,
while those of B-B’ in (d) with 2-rows are rarely broadened. Here,
(UM, LM) in (a) and (b) refer to the phasings between rows, and
in (c) and (d) refers the phase difference between upper and lower
rows without mid-row.
Fig. 7 Comparison of divertor heat flux measurement
and field-line-tracing calculation during rotating
RMP. Shown in (a) is the time evolution of the
measured divertor heat during “distorted” IMC
during ELM-crash-suppression. On the other hand,
shown in (b) is the contour of minimum flux surface
calculated in a field-line-tracing, which suggests the
high heat flux would be equivalent to deeper RMP-
field penetration. Note that the dashed magenta box
appears quite similar to the measured heat flux,
which automatically discredits the deep penetration
field near Rdivertor ~ 1.44 m in the simulation, while
the vertical dashed line refers to a typical IR camera
location in KSTAR without the presence of rotating
RMP. The weakly striated pattern in the region A in
(b) matches well with the measurement in (a).
EX7-1
unperturbed plasma (i.e. an exponential power profile decay length of q). The edge pedestal profiles are
assumed with a typical pedestal width = 0.02 m and Tped = 500 eV, while the separatrix temperature is
typically characterized by Tsep = 100 eV. To circumvent a lack of accurate edge density profile measurement in
KSTAR, we assume a ratio of pedestal and separatrix density of nped/nsep = 3-4, based on tokamak experiences.
Here, a typical power decay length is assumed to be q = 2 mm in the KSTAR plasmas, as characterized in
Figure 6. For simplicity, both density and temperature profiles are assumed to increase linearly in the pedestal
region from the separatrix, as the radial position move inwards into the plasma towards the pedestal top:
𝑇(𝑅) = 𝑇𝑠𝑒𝑝 +𝑇𝑝𝑒𝑑 − 𝑇𝑠𝑒𝑝
∆(𝑅𝑠𝑒𝑝 − 𝑅𝑚𝑖𝑑) (1)
𝑛(𝑅) = 𝑛𝑠𝑒𝑝 +𝑛𝑝𝑒𝑑 − 𝑛𝑠𝑒𝑝
∆(𝑅𝑠𝑒𝑝 − 𝑅𝑚𝑖𝑑) (2)
where R is the major radius at the outer midplane, Rsep and Rped are the separatrix and pedestal locations at the
outer midplane respectively, along with ( = Rsep - Rped) and Rped ≤ R ≤ Rsep.
The normalized magnetic flux can be related to Rsep – R by a linear expression or mapped by unperturbed
equilibrium information:
N = 1 + C (R-Rsep) (3)
where N > 1 corresponds to the points in the SOL and N < 1 corresponds to points in the edge plasma for the
unperturbed plasma.
Assuming that all the edge profiles become available, the heat flux profile at the divertor under the 3-D fields
can be specified as (normalized to 1 at R = Rsep):
A. R ≥ Rsep
𝑞𝑑𝑖𝑣(𝑅) = 𝑒(𝑅𝑠𝑒𝑝 − 𝑅)
𝜆𝑞 (4)
B. R ≤ Rsep
In this case the heat flux depends on the plasma T(R) and n(R) from the expressions above and the transport
along the field line are assumed to be either sheath-limited (qdiv ~ nT3/2) or conduction-limited (qdiv ~ T7/2).
So, the following two expressions can be considered for R ≤ Rsep
B.1. Sheath-limited heat flux
𝑞𝑑𝑖𝑣(𝑅) = 𝑛(𝑅) 𝑇(𝑅)
32⁄
𝑛𝑠𝑒𝑝 𝑇𝑠𝑒𝑝3/2 (5.1)
B.2. Conduction-limited heat flux
𝑞𝑑𝑖𝑣(𝑅) = 𝑇(𝑅)
72⁄
𝑇𝑠𝑒𝑝7/2 (5.2)
4.2 Divertor heat flux specification for the 3-D field impact assessment on striation pattern
The field-line-tracing calculation has been successfully conducted to understand the divertor heat flux striation
pattern in KSTAR[8]. A typical comparison between experiments and simulation is the connection length
calculation. However, since the correlation between core plasma and divertor needs to be made under the 3-D
field environment, a more adequate quantity could be the minimum N, where 3-D field line may penetrate to
core plasma ergodically. Here, the field-line-tracing calculation has been performed based on the perturbed 3-D
magnetic field using the IPEC[9]. Figure 7 illustrates such an example of field line calculation of N, min, with a
divertor heat flux striation pattern in experiments under “distorted” IMC. In comparison, some striations outside
the magenta box in Figure 7 (b) do not correspond to any meaningful counterparts in the experimental results. In
fact, it is deemed necessary for us to ignore such spurious field line penetration in the rest of analysis (e.g. the
narrow spikes near Rdiv ~1.445 m, next to the near-SOL peaks in Figure 8). Based on the modeling and field-
line-tracing calculations, Figure 8 summarizes the simulation results on both 3-row IMC (with ‘toward’ phasing)
and 2-row RMPs. In general, the conduction-limited model appears more peaked than the sheath-limited model,
which may be attributable to the difference of temperature powers between two models (i.e. T7/2 vs T3/2). Despite
quite a simple modeling, the field line tracing calculation shows the reduction of the divertor heat fluxes with 3-
row IMC, reasonably consistent with the experimental observations [e.g. Comparison of Figure 6 (a) with
Figure 8 (a)]. However, once the near-SOL peak is normalized, virtually no broadening can be seen, as shown in
the conduction-limited model results in Figure 8 (b). Even if the 2nd peaks (near Rdiv ~ 1.455 m) are included in
determining the width of the peaks, it does not seem to be adequate to predict any broadening using field-line-
tracing alone. As for 2-row RMPs, the field-line-tracing does not differentiate the variation of phasing at all. In a
way, this is understandable, in that a linear simulation, based on both IPEC and field-line-tracing, may not
adequately describe the non-linear phenomena, such as RMP-driven, ELM-crash-suppression. Of course, the 3-
D field requirement necessary for RMP-driven, ELM-crash-suppression can be linearly predicted, as
successfully demonstrated in KSTAR experiments[10].
IN et al.
7
5. PROGRESS IN
THE
COMPATIBILITY
STUDY OF ELM-
CRASH-
SUPPRESSION
WITH DETACHED
PLASMAS
Since the main
focus of divertor
heat flux dispersal
would be the
redistribution of the
peaked near-SOL
heat flux, the 3-D
heat flux
broadening is quite
favourable to the
choice of 3-rows in
ITER, instead of 2-
rows. However, we
are cautiously
aware of the
expectation of
completely
different
broadening
characteristics, which
might take place in
partially detached
plasmas in ITER[11].
Thus, it has been a high-
priority research theme
in KSTAR to investigate
whether RMP-driven,
ELM-crash-suppression
would be compatible
with detached plasmas.
Although a fully
detached plasma under
RMP has not been
obtained yet, we were
able to greatly reduce
heat flux at q95=3.8 using n=2 RMPs in high density plasmas, as shown in Figure 9. THis
6. DISCUSSION AND SUMMARY
The ITER-like intentionally misaligned configuration (IMC) has been successfully demonstrated to be not only
compatible with ELM-crash-suppression, but also promising in broadening the divertor heat fluxes in a wider
area. Although the choice of 3-row ITER RMP is greatly meritorious in this aspect, the physics question about
the broadening mechanism needs to be further clarified. While the IMC with “away” phasing greatly benefited
from a global ‘kink-resonance’ that would interact with edge RMP coupling [5], it remains to be answered what
causes the IMC with “toward” phasing to be similarly accompanied by divertor heat flux broadening. Based on
Fig. 9 Comparison of high (red) and low (black) density plasmas during n=2 RMP-
driven, ELM-suppression at q95=3.4. Shown are (a) the key physics parameters and (b)
divertor heat flux profiles for each discharge.
Fig. 8 Field-line-tracing simulation results with conduction-limited (C) and sheath-limited (S)
models (as described in Section 4) with 3-row and 2-row IMCs during ELM-crash-suppression
respectively. Shown on the left in (a) and (c) are the profiles of toroidally-averaged divertor
heat flux in each IMC, in comparison with a typical rotating RMP with n = 1, +90° phasing
(red) with 3-rows in (a) and -90° phasing with 2-rows in (c) respectively. On the right are the
corresponding normalized and enlarged shapes of divertor heat flux at each configuration. Here,
6, 9, 12 and 15 secs correspond to 0° , 5° 10° , and 15° of misalignment from the reference
phasing respectively.
EX7-1
a simple edge modeling, both conduction- and sheath-limited models appear reasonably consistent with the 3-
row IMC heat flux reduction, as the degree of misalignment from the reference phasing increases. Nonetheless,
the field-line-tracing alone does not seem to be adequate to predict the divertor heat flux broadening, suggesting
the need of more comprehensive non-linear simulation. In the meantime, a more sophisticated edge pedestal
modeling beyond a simple linear modeling may be an intermediate step to test the validity of both conduction-
and sheath-limited models. One of the critically important questions goes to a physics issue of whether or not
RMP-driven, ELM-crash-suppression would be compatible with detached plasmas. Since the increase of gas
puffing is typically accompanied by not only the density increase but also collisionality, a common practice to
prefer a low collisionality plasma for ELM-crash-suppression directly conflicts with the methodology to access
the detached plasma. Considering that the wall conditions of the detached plasmas (expected in ITER) are vastly
different from those of attached plasmas (as seen in KSTAR), the experimental demonstration, as well as
theoretical assessment, is in urgent need.
In summary, KSTAR has demonstrated ITER-like 3-row RMPs could be intentionally misaligned to disperse
divertor heat fluxes in a wider area during ELM-crash-suppression, while minimizing EM loads on RMP coils.
The ITER-like 3-row IMCs were found not only to have been compatible with the ELM-crash-suppression, but
also to have broadened the near-SOL divertor heat flux, which were not seen with 2-row RMPs so far. Although
the compatibility of ELM-crash-suppression with detached plasma has not been confirmed yet, significantly
reduced divertor heat flux was measured in high density ELM-crash-suppressed plasmas. In support of the ITER
RMP system, the remaining physics uncertainties will be further clarified using the 3-row IVCCs in KSTAR.
ACKNOWLEDGEMENTS
This work was supported by the Korean Ministry of Science and ICT for the KSTAR project (NFRI-EN1801-9),
National Research Fund (NRF-2014M1A7A1A03029865), and the 2018 UNIST research fund (1.180056.01),
as well as through active collaboration with PPPL and ORNL. We acknowledge all the KSTAR Team members
that have led the successful operations throughout the 3-D physics experiments.
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