“Development of 3-D Divertor Solutions for Stellarators Through Coordinated Domestic and International Research”
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Plasma-Materials and Divertor Options for Fusion
Plasma-Materials and Divertor Options for Fusion Presented to: National Academy of Sciences Panel A Strategic Plan for U.S. Burning Plasma Research J. Rapp ORNL is managed by UT-Battelle for the US Department of Energy Lifetime of divertor will deterimine fusion reactor availability TF coils Coolant manifold (permanent) Upper ports (modules and coolant) Blanket Cost of modules electricity is 5-6 yrs lifetime proportional 0.6 to (1/A) Central ports (modules) Vacuum vessel 70cm Cool shield (permanent) 30cm Divertor plates (permanent) Lower ports 2 yrs lifetime goal (divertor) Main driver of scheduled maintenance: divertor (and blanket) 2 Juergen Rapp Outline • Plasma-Material Interaction (PMI) challenges • Potential Plasma-Facing Materials (PFMs) and Components (PFCs) • Current status of U.S. PMI research • Facilities needed for the development of PFCs • Strategic elements to accelerate U.S. burning plasma research • A proposed high-level R&D program and roadmap for PMI 3 Juergen Rapp Outline • Plasma-Material Interaction (PMI) challenges • Potential Plasma-Facing Materials (PFMs) and Components (PFCs) • Current status of U.S. PMI research • Facilities needed for the development of PFCs • Strategic elements to accelerate U.S. burning plasma research • A proposed high-level R&D program and roadmap for PMI 4 Juergen Rapp Challenges for materials: fluxes and fluence, temperatures JET ITER FNSF Fusion Reactor 50 x divertor ion fluxes 5000 x divertor ion fluence up to 5 x ion fluence 106 x neutron fluence (1dpa) up to 100 x neutron fluence (150dpa) -
A European Success Story the Joint European Torus
EFDA JET JETJETJET LEAD ING DEVICE FOR FUSION STUDIES HOLDER OF THE WORLD RECORD OF FUSION POWER PRODUCTION EXPERIMENTS STRONGLY FOCUSSED ON THE PREPARATION FOR ITER EXPERIMENTAL DEVICE USED UNDER THE EUROPEAN FUSION DEVELOPEMENT AGREEMENT THE JOINT EUROPEAN TORUS A EUROPEAN SUCCESS STORY EFDA Fusion: the Energy of the Sun If the temperature of a gas is raised above 10,000 °C virtually all of the atoms become ionised and electrons separate from their nuclei. The result is a complete mix of electrons and ions with the sum of all charges being very close to zero as only small charge imbalance is allowed. Thus, the ionised gas remains almost neutral throughout. This constitutes a fourth state of matter called plasma, with a wide range of unique features. D Deuterium 3He Helium 3 The sun, and similar stars, are sphe- Fusion D T Tritium res of plasma composed mainly of Li Lithium hydrogen. The high temperature, 4He Helium 4 3He Energy U Uranium around 15 million °C, is necessary released for the pressure of the plasma to in Fusion T balance the inward gravitational for- ces. Under these conditions it is pos- Li Fission sible for hydrogen nuclei to fuse together and release energy. Nuclear binding energy In a terrestrial system the aim is to 4He U produce the ‘easiest’ fusion reaction Energy released using deuterium and tritium. Even in fission then the rate of fusion reactions becomes large enough only at high JG97.362/4c Atomic mass particle energy. Therefore, when the Dn required nuclear reactions result from the thermal motions of the nuclei, so-called thermonuclear fusion, it is necessary to achieve u • extremely high temperatures, of at least 100 million °C. -
Analysis of Equilibrium and Topology of Tokamak Plasmas
ANALYSIS OF EQUILIBRIUM AND TOPOLOGY OF TOKAMAK PLASMAS Boudewijn Philip van Millig ANALYSIS OF EQUILIBRIUM AND TOPOLOGY OF TOKAMAK PLASMAS BOUDEWHN PHILIP VAN MILUGEN Cover picture: Frequency analysis of the signal of a magnetic pick-up coil. Frequency increases upward and time increases towards the right. Bright colours indicate high spectral power. An MHD mode is seen whose frequency decreases prior to a disruption (see Chapter 5). II ANALYSIS OF EQUILIBRIUM AND TOPOLOGY OF TOKAMAK PLASMAS ANALYSE VAN EVENWICHT EN TOPOLOGIE VAN TOKAMAK PLASMAS (MET EEN SAMENVATTING IN HET NEDERLANDS) PROEFSCHRIFT TER VERKRUGING VAN DE GRAAD VAN DOCTOR IN DE WISKUNDE EN NATUURWETENSCHAPPEN AAN DE RUKSUNIVERSITEIT TE UTRECHT, OP GEZAG VAN DE RECTOR MAGNIFICUS PROF. DR. J.A. VAN GINKEL, VOLGENS BESLUTT VAN HET COLLEGE VAN DECANEN IN HET OPENBAAR TE VERDEDIGEN OP WOENSDAG 20 NOVEMBER 1991 DES NAMIDDAGS TE 2.30 UUR DOOR BOUDEWUN PHILIP VAN MILLIGEN GEBOREN OP 25 AUGUSTUS 1964 TE VUGHT DRUKKERU ELINKWIJK - UTRECHT m PROMOTOR: PROF. DR. F.C. SCHULLER CO-PROMOTOR: DR. N.J. LOPES CARDOZO The work described in this thesis was performed as part of the research programme of the 'Stichting voor Fundamenteel Onderzoek der Materie' (FOM) with financial support from the 'Nederlandse Organisatie voor Wetenschappelijk Onderzoek' (NWO) and EURATOM, and was carried out at the FOM-Instituut voor Plasmafysica te Nieuwegein, the Max-Planck-Institut fur Plasmaphysik, Garching bei Munchen, Deutschland, and the JET Joint Undertaking, Abingdon, United Kingdom. IV iEstos Bretones -
Formation of Hot, Stable, Long-Lived Field-Reversed Configuration Plasmas on the C-2W Device
IOP Nuclear Fusion International Atomic Energy Agency Nuclear Fusion Nucl. Fusion Nucl. Fusion 59 (2019) 112009 (16pp) https://doi.org/10.1088/1741-4326/ab0be9 59 Formation of hot, stable, long-lived 2019 field-reversed configuration plasmas © 2019 IAEA, Vienna on the C-2W device NUFUAU H. Gota1 , M.W. Binderbauer1 , T. Tajima1, S. Putvinski1, M. Tuszewski1, 1 1 1 1 112009 B.H. Deng , S.A. Dettrick , D.K. Gupta , S. Korepanov , R.M. Magee1 , T. Roche1 , J.A. Romero1 , A. Smirnov1, V. Sokolov1, Y. Song1, L.C. Steinhauer1 , M.C. Thompson1 , E. Trask1 , A.D. Van H. Gota et al Drie1, X. Yang1, P. Yushmanov1, K. Zhai1 , I. Allfrey1, R. Andow1, E. Barraza1, M. Beall1 , N.G. Bolte1 , E. Bomgardner1, F. Ceccherini1, A. Chirumamilla1, R. Clary1, T. DeHaas1, J.D. Douglass1, A.M. DuBois1 , A. Dunaevsky1, D. Fallah1, P. Feng1, C. Finucane1, D.P. Fulton1, L. Galeotti1, K. Galvin1, E.M. Granstedt1 , M.E. Griswold1, U. Guerrero1, S. Gupta1, Printed in the UK K. Hubbard1, I. Isakov1, J.S. Kinley1, A. Korepanov1, S. Krause1, C.K. Lau1 , H. Leinweber1, J. Leuenberger1, D. Lieurance1, M. Madrid1, NF D. Madura1, T. Matsumoto1, V. Matvienko1, M. Meekins1, R. Mendoza1, R. Michel1, Y. Mok1, M. Morehouse1, M. Nations1 , A. Necas1, 1 1 1 1 1 10.1088/1741-4326/ab0be9 M. Onofri , D. Osin , A. Ottaviano , E. Parke , T.M. Schindler , J.H. Schroeder1, L. Sevier1, D. Sheftman1 , A. Sibley1, M. Signorelli1, R.J. Smith1 , M. Slepchenkov1, G. Snitchler1, J.B. Titus1, J. Ufnal1, Paper T. Valentine1, W. Waggoner1, J.K. Walters1, C. -
Plasma Stability and the Bohr - Van Leeuwen Theorem
NASA TECHNICAL NOTE -I m 0 I iii I nE' n z c * v) 4 z PLASMA STABILITY AND THE BOHR - VAN LEEUWEN THEOREM by J. Reece Roth Lewis Research Center Cleueland, Ohio NATIONAL AERONAUTICS AND SPACE ADMINISTRATION WASHINGTON, D. C. APRIL 1967 I ~ .. .. .. TECH LIBRARY KAFB, NM I llllll Illlll lull IIM IIllIll1 Ill1 OL3060b NASA TN D-3880 PLASMA STABILITY AND THE BOHR - VAN LEEWEN THEOREM By J. Reece Roth Lewis Research Center Cleveland, Ohio NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sale by the Clearinghouse for Federal Scientific and Technical Information Springfield, Virginia 22151 - CFSTI price $3.00 CONTENTS Page SUMMARY.- ........................................ 1 INTRODUCTION-___ ..................................... 2 THE BOHR - VAN LEEUWEN THEOREM ....................... 3 RELATION OF THE BOHR - VAN LEEUWEN THEOREM TO CONVENTIONAL MACROSCOPIC THEORIES OF PLASMA STABILITY ................ 3 The Momentum Equation .............................. 3 The Conventional Magnetostatic and Hydromagnetic Theories .......... 4 The Bohr - van Leeuwen Theorem. ........................ 7 Application of the Bohr - van Leeuwen Theorem to Plasmas ........... 9 The Bohr - van Leeuwen Theorem and the Literature of Plasma Physics .... 10 PLASMA CURRENTS ................................. 11 Assumptions of Analysis .............................. 11 Sources of Plasma Currents ............................ 12 Net Plasma Currents. ............................... 15 CHARACTERISTICS OF PLASMAS SATISFYING THE BOHR - VAN LEEUWEN THEOREM ..................................... -
Steady State and Transient Power Handling in JET G.F.Matthews* on Behalf of the JET EFDA Exhaust Physics Task Force and JET EFDA Contributors+ +See Annex of J
Steady State and Transient Power Handling in JET G.F.Matthews* on behalf of the JET EFDA Exhaust Physics Task Force and JET EFDA Contributors+ +See annex of J. Pamela et al, "Overview of JET Results", Fusion Energy 2002 (Proc. 19th Int. Conf. Lyon, 2002),IAEA, Vienna. *Euratom/UKAEA Fusion Association, Culham Science Centre, Abingdon, Oxon. OX14 3DB,UK. E-mail: [email protected] Abstract. Steady state and transient power deposition profiles have been measured in the JET MIIGB divertor using improved diagnostics techniques involving the use of fast infra-red, thermocouples and Langmuir probe arrays. In unfuelled type I ELMy H-modes a very narrow power profile is observed at the outer target which we associate with the ion channel. Systematic parameter scans have been carried out and our analysis shows that the average power width scaling is consistent with a classical dependence of perpendicular transport in the SOL. Using the fast IR capability the factors such as rise time, broadening, variability and in/out asymmetry have been studied and lead to the conclusion that type I ELMs in ITER may fall just below the material ablation limits. JET disruptions are very different from type I ELMs in that only a small fraction of the thermal energy reaches the divertor and what does arrive is distributed uniformly over the divertor area. This is very different from the current ITER assumption which puts most of the energy from the thermal quench onto the divertor strike points. 1. Introduction The actively cooled divertor target for ITER has been tested up to a surface power loading of 25MWm-2 but the planned operating point is around 10MWm-2 to allow for excursions. -
The Pumped Divertor the NEW PHASE of JET B.E
The Pumped Divertor THE NEW PHASE OF JET B.E. Keen and M.L. Watkins and the JET Team JET Joint Undertaking, Abingdon, Oxford, UK Associate Member of EPS The pumped divertor experiment, in demonstrating before full deuterium-tritium operation an effective method of impurity control, aims to provide essential design data for a Next Step tokamak fusion device. The basic principle of the fusion pro Switzerland and Sweden. By mid-1983, by careful design of the targets and speci cess is the fusing of light nuclei to form the construction of JET, its power supplies fic operational techniques, but is limited, heavier ones and the accompanying re and buildings were completed on sche ultimately, by an unacceptably high influx lease of substantial energy. For a fusion dule and broadly to budget and the prog of impurities. The fourth area of work had reactor, there are several possible fusion ramme started. been started by earlier studies of energetic reactions, but the one that is easiest to JET is the largest project in the coordi particles produced as fusion products or achieve is that between the deuterium and nated programme of EURATOM, whose by ion cyclotron resonance heating tritium isotopes of hydrogen. This D-T fusion programme is designed to lead ulti (ICRH). It has now been addressed further reaction is : mately to the construction of an energy by the first tokamak plasma experiments D + T → 4He + neutrons + 17.6 MeV. producing reactor. Its strategy is based on in D-T mixtures. These results are presen At the temperatures needed for this reac the sequential construction of major ap ted briefly in the following sections. -
Modeling and Control of Plasma Rotation for NSTX Using
PAPER Related content - Central safety factor and N control on Modeling and control of plasma rotation for NSTX NSTX-U via beam power and plasma boundary shape modification, using TRANSP for closed loop simulations using neoclassical toroidal viscosity and neutral M.D. Boyer, R. Andre, D.A. Gates et al. beam injection - Topical Review M S Chu and M Okabayashi To cite this article: I.R. Goumiri et al 2016 Nucl. Fusion 56 036023 - Rotation and momentum transport in tokamaks and helical systems K. Ida and J.E. Rice View the article online for updates and enhancements. Recent citations - Design and simulation of the snowflake divertor control for NSTX–U P J Vail et al - Real-time capable modeling of neutral beam injection on NSTX-U using neural networks M.D. Boyer et al - Resistive wall mode physics and control challenges in JT-60SA high scenarios L. Pigatto et al This content was downloaded from IP address 128.112.165.144 on 09/09/2019 at 19:26 IOP Nuclear Fusion International Atomic Energy Agency Nuclear Fusion Nucl. Fusion Nucl. Fusion 56 (2016) 036023 (14pp) doi:10.1088/0029-5515/56/3/036023 56 Modeling and control of plasma rotation for 2016 NSTX using neoclassical toroidal viscosity © 2016 IAEA, Vienna and neutral beam injection NUFUAU I.R. Goumiri1, C.W. Rowley1, S.A. Sabbagh2, D.A. Gates3, S.P. Gerhardt3, M.D. Boyer3, R. Andre3, E. Kolemen3 and K. Taira4 036023 1 Department of Mechanical and Aerospace Engineering, Princeton University, Princeton, NJ 08544, USA I.R. Goumiri et al 2 Department of Applied Physics and Applied Mathematics, -
An Overview of the HIT-SI Research Program and Its Implications for Magnetic Fusion Energy
An overview of the HIT-SI research program and its implications for magnetic fusion energy Derek Sutherland, Tom Jarboe, and The HIT-SI Research Group University of Washington 36th Annual Fusion Power Associates Meeting – Strategies to Fusion Power December 16-17, 2015, Washington, D.C. Motivation • Spheromaks configurations are attractive for fusion power applications. • Previous spheromak experiments relied on coaxial helicity injection, which precluded good confinement during sustainment. • Fully inductive, non-axisymmetric helicity injection may allow us to overcome the limitations of past spheromak experiments. • Promising experimental results and an attractive reactor vision motivate continued exploration of this possible path to fusion power. Outline • Coaxial helicity injection NSTX and SSPX • Overview of the HIT-SI experiment • Motivating experimental results • Leading theoretical explanation • Reactor vision and comparisons • Conclusions and next steps Coaxial helicity injection (CHI) has been used successfully on NSTX to aid in non-inductive startup Figures: Raman, R., et al., Nucl. Fusion 53 (2013) 073017 • Reducing the need for inductive flux swing in an ST is important due to central solenoid flux-swing limitations. • Biasing the lower divertor plates with ambient magnetic field from coil sets in NSTX allows for the injection of magnetic helicity. • A ST plasma configuration is formed via CHI that is then augmented with other current drive methods to reach desired operating point, reducing or eliminating the need for a central solenoid. • Demonstrated on HIT-II at the University of Washington and successfully scaled to NSTX. Though CHI is useful on startup in NSTX, Cowling’s theorem removes the possibility of a steady-state, axisymmetric dynamo of interest for reactor applications • Cowling* argued that it is impossible to have a steady-state axisymmetric MHD dynamo (sustain current on magnetic axis against resistive dissipation). -
Lyra' Divertor
ENERGY AND PARTICLE CONTROL CHARACTERISTICS OF THE ASDEX UPGRADE `LYRA' DIVERTOR M. Kaufmann, H-S. Bosch, A. Herrmann, A. Kallenbach, K. Borrass, A. Carlson, D. Coster, J.C. Fuchs, J. Gafert, K. Lackner, J. Neuhauser, R. Schneider, J. Schweinzer, W. Suttrop, W. Ullrich, U. Wenzel, and ASDEX Upgrade team Max-Planck-Institut fÈurPlasmaphysik, EURATOM-IPP Association, Garching und Berlin, Germany Abstract In 1997 the new `LYRA' divertor went into operation at ASDEX Upgrade and the neutral beam heating power was increased to 20 MW by installation of a second injector. This leads to the relatively high value of P/R of 12 MW/m. It has been shown that the ASDEX Upgrade LYRA divertor is capable of handling such high heating powers. Mea- surements presented in this paper reveal a reduction of the maximum heat ¯ux in the LYRA divertor by more than a factor of two compared to the open Divertor I. This reduction is caused by radiative losses inside the divertor region. Carbon radiation cools the divertor plasma down to a few eV where hydrogen radiation losses become signi®cant. They are increased due to an effective re¯ection of neutrals into the hot separatrix region. B2-Eirene modelling of the performed experiments supports the experimental ®ndings and re®nes the understanding of loss processes in the divertor region. 1. INTRODUCTION The width of the scrape-off layer (SOL) does not necessarily increase in proportion to the size of the device. This poses severe problems for the power exhaust in a fusion reactor. If we take ITER as described in the ®nal design report (FDR) [1], a power ¯ow across the separatrix in the order of 100 to 150 MW might be needed to stay in the H-mode [2]. -
Coupling Optimization Experiment on HL-2A Based on Passive-Active Multijunction Antenna for 3.7Ghz Lower Hybrid System
42nd EPS Conference on Plasma Physics P5.137 Coupling optimization experiment on HL-2A based on Passive-Active Multijunction antenna for 3.7GHz Lower Hybrid system Xingyu Bai, Hao Zeng, Bo Lu, Xiaolan Zou1, Roland Magne1, Annika Ekedahl1, Julien Hillairet1, Chao Wang, Jun Liang, He Wang, Yali Chen, Junwei He, Jieqiong Wang, Kun Feng and Jun Rao Southwestern Institute of Physics, Chengdu, China 1 CEA, IRFM, 13108 Saint Paul-lez-Durance, France System Introduction. A new Lower Hybrid Wave (LHW) system (3.7GHz/2MW/2s) has been built on HL-2A tokamak. A Passive-Active-Multijunction (PAM) concept antenna [1], [2] was designed and built, fed by 500kW × 4 TH2103A Klystrons, delivering ITER-relevant power density, i.e. 25MW/m2 at f = 3.7GHz [3],[4]. The antenna is designed to launch a peak parallel refractive index of N||=2.75 with a low theoretical Reflection Coefficient (RC), i.e. less than 1% [5], [6]. A specific gas puffing system for improving the antenna coupling and a set of Langmuir probes for antenna mouth density measurements are separately located on one side of the antenna each. An auxiliary vacuum system is installed at the rear of the antenna to improve the pumping efficiency. Vacuum leak tests and low power microwave scattering parameter measurements were done before the PAM antenna was installed on HL-2A, allowing the antenna to be conditioned at RF power of 100kW/100ms before starting plasma operation. Fig. 1: New LHW system(3.7GHz/2MW/2s)of HL- Fig. 2: PAM launcher was developed and installed, facing 2A. -
An Overview of Plasma Confinement in Toroidal Systems
An Overview of Plasma Confinement in Toroidal Systems Fatemeh Dini, Reza Baghdadi, Reza Amrollahi Department of Physics and Nuclear Engineering, Amirkabir University of Technology, Tehran, Iran Sina Khorasani School of Electrical Engineering, Sharif University of Technology, Tehran, Iran Table of Contents Abstract I. Introduction ………………………………………………………………………………………… 2 I. 1. Energy Crisis ……………………………………………………………..………………. 2 I. 2. Nuclear Fission ……………………………………………………………………………. 4 I. 3. Nuclear Fusion ……………………………………………………………………………. 6 I. 4. Other Fusion Concepts ……………………………………………………………………. 10 II. Plasma Equilibrium ………………………………………………………………………………… 12 II. 1. Ideal Magnetohydrodynamics ……………………………………………………………. 12 II. 2. Curvilinear System of Coordinates ………………………………………………………. 15 II. 3. Flux Coordinates …………………………………………………………………………. 23 II. 4. Extensions to Axisymmetric Equilibrium ………………………………………………… 32 II. 5. Grad-Shafranov equation (GSE) …………………………………………………………. 37 II. 6. Green's Function Formalism ………………………………………………………………. 41 II. 7. Analytical and Numerical Solutions to GSE ……………………………………………… 50 III. Plasma Stability …………………………………………………………………………………… 66 III. 1. Lyapunov Stability in Nonlinear Systems ………………………………………………… 67 III. 2. Energy Principle ……………………………………………………………………………69 III. 3. Modal Analysis ……………………………………………………………………………. 75 III. 4. Simplifications for Axisymmetric Machines ……………………………………………… 82 IV. Plasma Transport …………………………………………………………………………………. 86 IV. 1. Boltzmann Equations ……………………………………………………………………… 87 IV. 2. Flux-Surface-Average