1 6/13/2015 ARIES PULSAR STARLITE Overview of ARIES Physics Studies ARIES-I, ARIES-II/IV, ARIES-III [D- 3 He], Pulsar, ARIES-RS, ARIES-ST, ARIES-AT presented.

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1 6/13/2015 ARIES PULSAR STARLITE Overview of ARIES Physics Studies ARIES-I, ARIES-II/IV, ARIES-III [D- 3 He], Pulsar, ARIES-RS, ARIES-ST, ARIES-AT presented by S.C. Jardin PPPL For the ARIES Physics Team ARIES Program Review Aug UCSD

2 6/13/2015 ARIES PULSAR STARLITE Principal Collaborators S. Kaye, C. Kessel, J. Menard Princeton Plasma Physics Laboratory B.J. Lee, T.K. Mau, R. Miller, F. Najmabadi University of California at San Diego C. Bathke Los Alamos National Laboratory D. Ehst Argonne National Laboratory V. Chan, L. Lao, Y-R. LinLiu, B. Miller, T. Petrie, P. Politzer, R. Prater, M. Schaffer, G. Staebler, A.Turnbull General Atomics

3 6/13/2015 ARIES PULSAR STARLITE Outline Overview of the ARIES Physics Studies Some Physics Highlights and Lessons Learned from the ARIES studies Physics Figures of Merit allow comparison with existing tokamak database Impact on General R&D Summary and Conclusions

4 6/13/2015 ARIES PULSAR STARLITE - Overview - Features of The ARIES Studies Systems Code does not do all the physics analysis –Detailed MHD and CD analysis performed for each plasma regime –These detailed results are then incorporated into the systems code Physics Analysis is performed in enough depth to uncover critical issues and key dependencies –Some desirable physics features cannot be incorporated simultaneously with others...eg., highest  and highest I BS /I P –Some desirable physics regimes are not compatible with engineering constraints...eg., highest plasma  and  These considerations have led to the identification of preferred physics regimes –ARIES-RS/AT, ARIES-ST

5 6/13/2015 ARIES PULSAR STARLITE - Overview - Physics input in is in 5 key areas Detailed equilibrium and stability analysis* –Includes plasma startup, vertical control, etc Detailed bootstrap and current drive analysis* –Includes calculation of CD profiles and antenna design Confinement and profiles –“Experimental” profiles, ITER confinement scaling Divertors and heat removal –Compatible with engineering constraints Particle exhaust and fueling *these are gone into in the most depth

6 6/13/2015 ARIES PULSAR STARLITE -Overview - Comparison of the ARIES designs

7 6/13/2015 ARIES PULSAR STARLITE - Physics Highlights - Five Distinct Operating Regimes have been explored for Power-Plant potential ARIES-I.. First Stability –tradeoff between high-  and high-I BS / I P, –intermediate elongation is best ARIES-II/IV.. Second Stability –showed true benefit of “high q 0 ” 2 nd Stability was to reduce CD requirement, not to increase  PULSAR.. Pulsed Reactor –demonstrated that  is limited by ohmic profile constraint ARIES-RS/AT.. Reversed Shear –excellent reactor potential for RS comes from both high  and reduced CD requirements ST (Low-A).. Normal Conductors –first self-consistent stability and CD calculation of high-  and high-I BS / I P Low-A Equilibrium

8 6/13/2015 ARIES PULSAR STARLITE - Physics Highlights – Many Critical Issues and dependencies have been uncovered by the Power-Plant Studies MHD Regime: tradeoff  for I BS /I P (and alignment) and hence circulating power operate at 90% of  -limit to reduce disruption frequency severe constraints on close-fitting shell and n>0 feedback effect of ohmic-profiles on stable  in non-CD machine Plasma Shaping: plasma elongation limited by control-coil power and conductor location plasma triangularity restricted by divertor geometry Current Drive: need for efficient off-axis CD (other than LHCD)  -resonance's and absorption taken into account CD frequency also important for wall-plug efficiency minimize coverage of RF launchers to avoid affecting tritium breeding Divertors: radiated power needed to reduce power to divertor Confinement: Standard confinement scalings sufficient for most designs

9 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Non-Inductive current drive is very costly  I CD =  CD (P CD /n e R) I CD = Total non-inductively driven current (A) P CD = Power to plasma by CD system (W) n e = average density (in units of /m 3 ) R = major radius (m)  CD = CD figure of merit Theoretical calculations show  CD  T e n with 0.6 < n < 0.8 Highest values to date for  CD are 0.45 (JET with ICRF+LH) and 0.34 (JT-60 with LHCD). Note that for a Reactor with I P =20 MA, n e = 1.5 x 10 20, R = 8 m,  CD = 0.34, this gives P CD = 700 MW to the plasma. This is unrealistic for a 1000 MW Power plant, since wall plug power is much higher (several efficiencies involved) => most of the plasma current must be self-generated (bootstrap) for a non-inductive reactor

10 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - It’s  (i.e.  R 0 /a) that’s important for a SC design MHD Theory SC Reactors shieldTF coilPlasma CLCL R0R0 R 0 - 3a/2 a B T =  0 I TF /2  R is limited by it’s value at the edge of the TF coil, R ~ R 0 - 3a/2  = a/R  B T 2 Almost independent of  for B T at the TF coil held fixed MHD Figure of merit  Large aspect ratio expansion of MHD perturbed energy  W shows that  enters only as  (reduced MHD) 2. Troyon scaling may be written in dimensionless form as:  < C T S/(20q*) Here, the right hand side is independent of . C T = 3.5 is the Troyon coefficient, q* > 2 is the cylindrical safety factor, and S=(1+  2 )/2 is the shape factor. R BTBT Power Density: P ~  2 B T 4 = (  ) 2 (  B T 2 ) 2

11 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Summary of power-plant options Superseded by –RS/AT

12 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Decision Tree for Fusion Power Plant Design Can wall stabilization of kink modes be made to work in a reactor environment? ARIES-RS/AT ARIES-ST ARIES-I PULSAR ARIES-RS-NW ARIES-ST-NW PULSAR+CD NOYES

13 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Assume wall stabilization of kink-modes turns out to be practical Main difference between ARIES-RS/AT and ARIES-ST is choice of TF conductor 90+% Bootstrap Current wall to stabilize kink modes maximize  2 B 4 to ballooning CopperSC Optimizes at 1.2 < A < 1.6 ARIES-ST Optimizes at 2.5 < A < 5 ARIES-RS/AT

14 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - ARIES-ST and ARIES-RS/AT are closely related: Similar optimizations but different A = R/a Optimize pressure profile at f BS =99% to maximize  subject to ballooning stability n,T ~ p 1/2 A = 1.6  = 3.4  = 56%  N = 8.2 A = 3.3  = 2.5  = 14%  N = 6 (note: actual ARIES- RS/AT designs less aggressive at A=4.0,  =1.9/2.1,  N =4.8/5.4)

15 6/13/2015 ARIES PULSAR STARLITE Troyon Limit Bootstrap fraction Toroidal Field Power Dissipated in TF Coil Fusion Power Engineering Q - Lessons Learned - Simple scaling relations show ARIES-ST is good aspect ratio for Copper Tokamak:

16 6/13/2015 ARIES PULSAR STARLITE Optimizes at :  large  N, large  large B MAX, large R  N and  are set by stability limits and their allowable values increase at low A =  -1 We can approximate MHD stability scalings in the range 1.2 < A < 3 by:  N ~ (1-  ) -1/2, (1+  2 ) ~ (1-  ) -1/2  Q E optimizes at intermediate A =   ~ Lessons Learned - Physics Parameters should be chosen to optimize Q E within acceptable limits.

17 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Reversed Shear such as ARIES-RS/AT is preferred configuration for SC tokamak with stabilizing walls Ozeki, Turnbull, Kessel, and others showed non-monotonic q-profile good for several reasons: Stable up to C T = (or higher) Bootstrap current aligns well with equilibrium current, allowing bootstrap fractions approaching 1.0 => both high  and high I BS /I P possible simultaneously Transport seems to be consistent with profiles required A=R/a=4, I BS /I P =.88 (.92),  =5% (9%) No strong dependence on Aspect Ratio many questions remain for practical realization requires wall stabilization of the kink mode can these favorable profiles be maintained ? J q 0r/a 1 Troyon Limit

18 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Decision Tree for Fusion Power Plant Design Can wall stabilization of kink modes be made to work in a reactor environment? ARIES-RS/AT ARIES-ST ARIES-I PULSAR ARIES-RS-NW ARIES-ST-NW PULSAR+CD NOYES

19 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Assume wall stabilization of kink-modes is not practical Main difference between other designs is choice of current drive options, bootstrap fraction and steady state maximize  2 B 4 (or  ) to ballooning and kink modes maximize  B = n e I P R/P CD for SS pulsed Steady state PULSAR (not AT) PULSAR+CD ARIES-I ARIES-RS-NW ARIES-ST-NW  too low  N (low  and I BS /I P )

20 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Comments on the need for wall stabilization Several “advanced tokamak” options should be considered and prototyped even if wall stabilization of kink modes is not feasible ARIES-Isteady state with conventional q profile ARIES-RS-NWsteady state with reversed q-profile PULSAR + CDpulsed (ITER-like) with CD Ultimately, the preferred option will be the one that is: – most reliable (ie, disruption and other failure mode free) – has adequate confinement – has high enough fusion power density  2 B 4 – low enough recirculating power

21 6/13/2015 ARIES PULSAR STARLITE - Lessons Learned - Pulsed or Steady State? Advantages of Pulsed Inductive current drive very efficient in Amps/Watt »low recirculating power »not constrained to high  P Heating systems can be optimized for heating to ignition, not CD Advantages of Steady State Continuous operation »magnet stresses can be higher(~2) »no need for OH coils & their power supplies »no need for energy storage »fewer disruptions Control of current profile »high  N and sawtooth free operation possible »possibility of 2 ND stab, rev shear, Low-A operation

22 6/13/2015 ARIES PULSAR STARLITE PULSAR design was purely inductive: 2 hr pulse q* NN A=3 A=5 A=4 Current profile determined from T and n profiles by stationary constraint with no CD except bootstrap: Optimizes at higher I P (lower  P ) than other designs to maximize  Optimization with some current drive added has not been done ie. PULSAR-CD T 0 / = 1.9 n 0 / = 1.3

23 6/13/2015 ARIES PULSAR STARLITE Physics Figures of Merit Provide Link between Power-Plant Studies and Base Program Reactor Design Theory Program Experimental Program Physics Figures of Merit Evaluate credibility What is Important What has been Achieved What to Demonstrate Physics Limits Stimulus for New Ideas

24 6/13/2015 ARIES PULSAR STARLITE Physics Figures of Merit In each of the 5 critical physics areas, we have identified key physics parameters that characterize the physics operating regime These provide a convenient way to assess present data base and progress towards reactor-grade parameter (1)MHD Stability:  and  P (2)Current Drive:  B = n e I P R / P CD vs T e (3)Heat Exhaust:P HEAT /R vs f RAD (4)Energy Confinement:  E /a 2  vs  (5)Helium Ash removal:  He * /  E vs  E /a 2 

25 6/13/2015 ARIES PULSAR STARLITE MHD Figure of Merit is  vs  P Need both high fusion power density and high bootstrap current simultaneously

26 6/13/2015 ARIES PULSAR STARLITE Current Drive Figure of Merit is  B vs T e  B = n e I P R / P CD But I P = I BS + I CD, = I CD /(1- f BS ) *improvement can be made by either operating at high f BS = I BS /I P or with efficient current drive I CD

27 6/13/2015 ARIES PULSAR STARLITE Power Handling FOM is P HEAT /R vs f RAD Need to demonstrate high radiation fraction and high power handling capability simultaneously

28 6/13/2015 ARIES PULSAR STARLITE Energy Confinement FOM is  E /a 2  vs  Note:  E /a 2  (H 89P /q*) 2 This is just nT  with the major dimensional parameters factored out, or the ITER L-mode scaling parameter with the dominant dependence on the current removed.

29 6/13/2015 ARIES PULSAR STARLITE Helium Ash removal:  He * /  E vs  E /a 2  Need adequate helium ash removal and good energy confinement performance simultaneously

30 6/13/2015 ARIES PULSAR STARLITE Impact on R&D The ARIES Physics studies have been published in refereed journals –Fusion Eng. Des 38: “Physics Basis for a reversed shear tokamak power plant”, (1997) –Fusion Eng. Des (submitted) “Physics basis for a spherical torus fusion power plant”, –Fusion Eng. Des (to appear 2000) “Physics basis for a tokamak fusion power plant” These Power Plant Studies have had a considerable effect on the base program –TPX & KSTAR design influenced significantly by ARIES –Reversed shear experiments motivated by Reactor potential (FED article referenced in several DIII reports and pub.) –NSTX and NCSX designs influenced by these studies –Motivation for ITER and FIRE Advanced Physics Modes

31 6/13/2015 ARIES PULSAR STARLITE Summary and Comments This program has produced optimized power plant designs consistent with detailed physics analysis Many important dependencies have been identified between physics regimes and engineering constraints Methods proposed for meeting these constraints have had a significant influence on the base program and on program planning Physics Figure of Merit activity provides an assessment of how close we are to having a prototype of a reactor-grade tokamak These studies provides a useful forum for new physics ideas to meet engineering constraints