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Reactor Configuration Development for ARIES-CS. L. P. Ku and the ARIES-CS Team Princeton Plasma Physics Laboratory Princeton University, Princeton, NJ 08543. Abstract. - PowerPoint PPT Presentation
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Reactor Configuration Development for ARIES-CS
L. P. Ku and the ARIES-CS Team
Princeton Plasma Physics Laboratory
Princeton University, Princeton, NJ 08543
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Abstract
• Progress has been made in developing new classes of quasi-axially symmetric configurations for ARIES-CS that have good particle confinement properties and good integrity of equilibrium flux surfaces at high .
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• For each new class of configurations, we have
designed coils to ensure that the new configurations are realizable and engineering-wise feasible.
– R/min (Coil-Plasma) ≤ 6– R/min (Coil-Coil) ≤ 10.
• The physics and coil properties of new configurations allow power producing reactors of ~2 GW be designed with R<9 m with DT fuels and with a full breeding blanket. The good quasi-axisymmetry limits the energy loss of to < 10%.
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• We showcase two new classes of
configurations
– Configurations with low magnetic shear even in the presence of large amount of bootstrap current.
– Configurations of very low aspect ratios (A~2.5)
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What Is ARIES-CS
ARIES-CS is a four-year, multi-institution program to study compact stellarator reactor systems.
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F. Najmabadi, UCSD
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Goals of Configuration Design Study
• Identify plasma engineering issues relevant to a compact stellarator reactor
• Find configurations that are optimized with respect to the components critical to reactor performance
– Aspect ratios versus QA– loss and its minimization– Equilibrium and MHD limits– Integrity of flux surfaces
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Minimum requirements in configuration optimization for MHD stable QA plasmas at high are not well known at present. The following are “acceptance criteria” generally considered§.
• Maximum residues of non-axisymmetry in magnetic spectrum.– neo-classical transport << anomalous transport
• ovall allowable “noise” content < ~2%.• effective ripple in 1/ transport, -eff < ~1%
– ripple transport and energetic particle loss• energy loss < ~10%
– rotational damping (?)
• Stability beta limits based on linear, ideal MHD theories.– vertical modes
– interchange stability• V″~2-4%. LHD, CHS stable while having a hill.
1/
2
2
ext
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– ballooning modes• stable to infinite-n modes (eigenvalues calculated by COBRA code). LHD exceeds infinite-n results. High-n calculation typically gives higher limits.
– kink modes• stable to n=1 and 2 modes without a conducting wall (eigenvalues calculated by
Terpsichore code). W7AS results showed mode (2,1) saturation and plasma remained quiescent.
– tearing modes• d/ds > 0
• Equilibrium and equilibrium beta limits– Shafranov shift
– large islands associated with low order rational surfaces• flux loss due to all isolated islands < 5%
– overlapping of islands due to high shears associated with the bootstrap current• limit d/ds
< 1/22
Aa 2
§The ability to achieve our goals is often compromised by the conflicting demands of various constraints. Typically, we impose different weights depending upon the characteristics of a configuration we are looking for. There is also an issue of convergence and accuracy in numerical calculations.
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To establish minimum requirements for coil design optimization, we need more feedback from and iteration with systems analysis and engineering design. Presently, we include
• Coil design– coil to coil and coil to plasma separation
• R/min(c-c) < 12
• R/min(c-p) < 6
– radius of curvature and complexity• Bmax/B0 ~2.5 for 0.3 m x 0.3 m conductor @R~8 m.
– adequate space for pumping, diagnostics, plasma heating and maintenance
• R/out (c-p) < Ap (R/<a>)
Configuration Design Targets (Cont.)
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Methods of Exploring Configuration Space
• Broaden search of aspect ratio – rotational transform space, identifying regions endowed with particularly interesting features.
• Build sophisticated computational systems to design configurations and coils which target the physics and engineering goals*.
* See companion poster : Modular Coil Design for the Ultra-Low Aspect Ratio Quasi-Axially Symmetric Stellarator MHH2
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Plasma Optimization System
Initial “guess”. Plasma boundary represented as Fourier coefficients.
1) Select p, J profiles, , B, FP
2) Iota target
3) MHD stability target (Mercier, ballooning, kink)
4) Transport target (QA, ripple)
5) Coil target (complexity, current density)
1) Evaluate equilibrium (VMEC, NSTAB), 2) Jacobian calculations, 3) determine direction of descent, 4) perform functional minimization (Levenberg-Marquardt, GA).
Targets met?
Refined calculation and detailed analysis
Modify weights
Flux surface quality, islands healing, PIES
ballooningkink
transport
shape/position
coil complexity
Constraints/weights
No
Yes
loss
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I. SNS family of configurations
Plane and perspective views of last LCMS geometry and |B| in real space.
KJC167 – a showcase for essentially flat iota profile, demonstrating the existence of excellence of flux surface integrity
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Why low overall shear is of interest?• The integrity of equilibrium flux surfaces places a limit on the attainable
beta
– Shafranov shift– Formation of magnetic islands– Spacing between island chains and magnetic field stochasticity
• We generally require
– Shafranov shift
– large islands associated with low order rational surfaces• flux loss due to all isolated islands < 5%
– overlapping of islands due to high shears associated with the bootstrap current
• limit d/ds
< 1/2
2
Aa 2
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How flux surface integrity might be achieved in QAS?
• Bootstrap currents in QAS are expected to be of similar magnitude to those in tokamaks.– High magnetic shear possible
• Rotational transform crossing large number of rational surfaces likely
• Rational surfaces may be close to each other
• One solution is to carefully tailor the rotational transform profile– Select regions free of low order resonances– Shape the plasma such that the rising rotational transform
due to the bootstrap current is compensated for by the decreasing transform from the shaping.
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9/176/11
9/16
External transform from plasma shaping
Total transform including contribution from bootstrap current at 6% .
KJC167 is a 3 field-period, aspect ratio 6 configuration of the SNS family in which the iota profile is selected to minimize the impact of low order resonance on the flux surface integrity. In this case, the external iota has a strong negative shear, but the iota at operating is expected to have a small but positive shear in most of the plasma volume.
Shear ~5%
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Excellent quality of flux surfaces is observed in most of the plasma for KJC167 at 6% as seen below based on a PIES calculation.
m=16
PIES and VMEC solutions are consistent.
Equilibrium calculated by PIES @6% .
Equilibrium calculated by VMEC
Poincaré plot in r- at =0.
In Cartesian
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Minimizing non-axisymmetric residues and effective ripples resulted in good quasi-axisymmetry. The effective ripple @s=1 is only 0.35% at 6% and the overall “noise” is <2.5%. Loss of energy is ~8% in one slowing down time in our model calculation.
|B| on last LCMS in U-V space
Ovall “noise” content
0.5% ~2.5% @s=1
Eight major non-symmetric components in the magnetic spectrum plotted as function of normalized toroidal flux.
vacuum
With pressure at 6%
Effective ripple
componentssymmetric,energymagnetic
componentsicnonsymmetr,energymagneticnoise
ιm]φ)[n(mθcosBB mn
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KJC167 is stable to the m=1, n=0 vertical mode according to the Terpsichore calculation (no feedback control necessary) and is slightly unstable to both low and high-n internal modes at =4%.
Infinite-n ballooning modes (Cobra calculation) @Low-n modes • R/vA~0.001
P-profile
J-profile
Note: stability analyses were based on the pressure and current profiles given above. Profiles may be further optimized to improve MHD stabilities to both the local and global modes.
6%
5%
3%
2%
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KJC167 may be unstable to free-boundary modes for ~6% according to the Terpsichore calculation primarily due to the m=2, n=1 mode, but it could be made stable with more flux surface shaping to improve the local shear. It may also be made more stable by choosing more optimized pressure and current profiles.
N=1 N=0
• R/vA~0.15
Wall @3.5x plasma-vacuum interface
Plasma-wall interface
Rad
ial d
isp
lace
men
t ei
gen
fun
ctio
n
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A proposed design for the modular coils is to have 6 coils/period with coil aspect ratio R/min(C-P)~6. The example given here, KJC167-M05, based on equal coil currents, has smooth contours with small toroidal excursion.
Coil contours viewed on “U-V” plane of the winding surface in one field period.
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II. MHH2 Family of Configurations
Plane and perspective views of the last LCMS geometry and |B| in real space.
MHH2-K14 – a showcase for very low aspect ratio A~2.65 configuration having low field ripples and excellent confinement of particles.
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Why low aspect ratio is of interest?
• Fusion power, P, is inversely proportional to the square of plasma aspect ratio, A– A = R/<a>, R=major radius, <a>=average minor
radius– P B42R3/A2
• Lower A allows lower B or or R.– Smaller sized-reactor (R)– Less stress and power for magnets (B)– Less MHD stability issues ()
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MHH2-K14 is a configuration of the ultra-low A family with relatively simple shaping and optimized for quasi-axisymmetry at 5% without any other driven currents.
LCMS in four toroidal angles over half period. Rotational transform as function of toroidal flux.
External transform due to plasma shaping
Expected at 5% with NCSX-like pressure/current profile
Assumed in configuration optimization
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MHH2-K14 has reasonably good QA, but it is not as good as 1104. The B(2,1) and B(3,2) components remain to be significant in the magnetic spectrum. The loss of energy is still reasonable, being < 10% (~6% in one slowing down time in our model calculation).
Eight major non-symmetric components in the magnetic spectrum plotted as function of normalized toroidal flux.
|B| on last LCMS in U-V space
Max. “noise” content ~3.4% @s=1
(2,1)
(3,2)(0,2)
(0,1)
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r/a=0.5
r/a=0.7
|B| versus poloidal angle in radians along field lines starting @ =0, =0.
effevtive ripple (1/)
Plots of |B| along field lines show an increased amount of secondary ripples and the epsilon-effective (calculated by the NEO code) at the edge is now ~0.8%.
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A vacuum magnetic well, ~4% @ s=1, was imposed as one of the constraints in the configuration optimization.
Magnetic well depth as function of normalized toroidal flux.
From plasma shaping. Well depth=3.8% @s=1.
Total @ 5% , p (1-s1.5)1.5
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But it is slightly unstable to both low- and high-n internal modes at =4%.
Infinite-n ballooning modes (Cobra calculation)
Low-n modes • R/vA~0.0009
5%
3%
2%
p (1-s1.5)1.5
Rad
ial d
isp
lace
men
t ei
gen
fun
ctio
n
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MHH2-K14 may be also unstable to the external modes for >5% according to the Terpsichore calculation, primarily due to modes of intermediate toroidal mode numbers 5 and 7.
• R/vA~0.12
Wall @3.5x plasma average minor radius
Plasma-wall interface
Ra
dia
l d
isp
lac
em
en
t e
ige
nfu
nc
tio
n
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No. of Coils: 8/period
Different Types of Coils: 4
R/min (coil-plasma)=5.5
R/min (coil-coil)=10.3
I /R-B (max)=0.32 MA/m-T
B(max)/B(0) = 1.9 for 0.4 m x 0.4 m conductor
A modular coil design for MHH2-K14 (K14LA). Details: see the companion paper.
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Summary & Conclusions• Taking advantage of recent experimental results which generally
showed that stellarator plasmas are more resilient to MHD perturbations than predicted by the linerar theories, we searched the rotational transform-aspect ratio space for configurations endowed with better quasi-axisymmetry, low -particale loss and better integrity of flux surfaces at high equilibrium beta.
• We have found configurations whose rotational transform have small but positive shear even with the presence of large amounts of bootstrap current, making the avoidance of low order rational surfaces possible. We have also found configurations in two field periods having very low aspect ratios, making reactors of high power density and smaller sizes likely.
• The most attractive configurations will ultimately be determined by results of systems optimization and other constraints arising from engineering designs. To this end, we have included in our effort also the initial coil designs to ensure the realizability of the configurations we found and have provided configuration and coil parameters to the systems study to allow a better understanding of the optimal parameters for a competitive power plant.