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International Collaboration On Lower Hybrid Current Drive Alain Bécoulet, Tuong Hoang,.
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International Collaboration On Lower Hybrid Current Drive Alain Bécoulet, Tuong Hoang, J.F. Artaud, Y.S. Bae, J. Belo, G. Berger-By, J.M. Bernard, Ph. Cara, A. Cardinali, C. Castaldo3, S. Ceccuzzi, R. Cesario, M. H. Cho, J. Decker, L. Delpech, H. J. Do, A. Ekedahl, J.Garcia, P. Garibaldi, M. Goniche, D. Guilhem, C. Hamlyn-Harris, J. Hillairet, Q.Y. Huang, F. Imbeaux, H. Jia, F. Kazarian, S.H. Kim, Y. Lausenaz, X. Litaudon, R. Maggiora, R. Magne, L. Marfisi, S. Meschino, D. Milanesio, F. Mirizzi, P. Mollard, W. Namkung, L. Pajewski, L. Panaccione, S. Park, H. Park, Y. Peysson, A. Saille, F. Samaille, G. Schettini, M. Schneider, P.K. Sharma, A. Tuccillo, O. Tudisco, G. Vecchi, R. Villari, K. Vulliez, Y. Wu, H.L. Yang, Q. Zeng
LHCD to sustain steady-state long pulses its possible mission in ITER H&CD mix Conceptual design of the ITER LHCD system: physics, technology Recent advances of Lower Hybrid Current Drive Technology R&D requirements for ITER Conclusions OUTLINE
Present Super Cond. devices Steady State or Long Pulse Operation? • “Steady-state”deals with physics timescales (MHD, energy confinement, current diffusion) • “Long Pulse Operation” refers to the integration of physics and technology
Long Pulse Operation simultaneouslyrequires • the long term operation of the magnetic configuration (current profile) • the long term operation of the kinetic configuration (temperature, confinement, particle content, rotation profiles) • the long term safe operation of the Coils, Plasma Facing Components, Structure Materials,H&CD systems, Diagnostics, … • a long term solution for fuel cycle (T)
HT-7 400s discharge [B. Wan 2009] Tore Supra6-min. discharge [Van Houtte 05] EAST one-minute discharge [B. Wan 09] All Tokamak Long Pulses are sustained by LHCD • Hours in TRIAM-1M • Minutes in EAST, HT-7 and Tore Supra (level of MA-MW)
Which Mission(s) for LHCD in ITER ? • Extend burn duration -> save Volt-seconds, from early plasma phases • Help Accessing and Sustaining Steady-State (Advanced Tokamak Physics) -> Drive far off-axis current, complementarily to Bootstrap Current, NBCD and ECCD.
(d) (c) (b) (a) LHCD Extending Burn Duration • Early application of LHCD (20MW) in the current ramp-up saves ~ 45Wb -> ~ 500s of burn duration [Kessel, Nucl. Fus. 2009; Kim, PPCF, 2009] • Decrease of plasma inductance li: li ≤ 0.3, beneficial for plasma vertical control [Hoang, Nucl. Fus. 2009] • All PF coil currents well within limits
up to45Wb (heating), preserved to the end of burn li decreases (off-axis LH current), li ≤ 0.3 All PF coil currents well within their limits Physics Design: Vs Saving
Propagation Pedestal LHCD Driving Off-Axis Current in ITER • Optimized N// index range: 1.8 – 2.2, OK for all scenarios • Current deposition range: 0.6<r/a<0.8 • Driven Current ~ 1MA (20 MW coupled / 14 MW in main wave lobe)
ILH RAY-STAR (Cardinali) C3PO/LUKE Simulated LHCD in ITER SS scenario (#4) • C3PO/LUKE/ALOHA: 14 MW of absorbed power (20MW injected) drive < 0.7MA disagrees with RAY-STAR (> 0.9MA) -> runs from other codes under same conditions
EC+IC+LH 21+20+13 MW RF-only H&CD Steady-state operation Steady-state Q ~7 / 3000scould be achieved • ECCD triggers and locks ITB position @ r/a ~ 0.5 • LHCD drives current @ 0.6-0.8 required for SS [Garcia PRL 08. This conference]
LHCD to sustain steady-state long pulses. Its possible mission in ITER Conceptual design of the ITER LHCD system: physics, technology Recent advances of Lower Hybrid Current Drive Technology R&D requirements for ITER Conclusions OUTLINE
A LHCD system for ITER • ITER Design Review and ITER STAC -> 20 MW LHCD system for ITER under consideration; for future Upgrade. • Five ITER partners joined efforts on conceptual design and feasibility study (voluntary basis): CN, EU (under EFDA), IN, KO, and US. • Feasibility Study initiated and coordinated by CEA/IRFM, under EFDA (“LH4IT” task) • Five Euratom-Associations (incl. 7 laboratories) involved in training young RF scientists/engineers on all aspects(“LITE” training programme)
The ‘LH4IT’ task Deliverable: pre-design document including conceptual design, costing, schedule, WBS, and R&D needs • CEA (coord.), ENEA, IST, POLITO, Univ. ROME 3, (CCFE, IPP-Prague, follow-up only) • Contribution from IO (HCD Department) • Support of International LHCD community: China, India, Korea, and US. Japan following-up.
Status Report • Physics Design updated (absorption, propagation, alpha particle issue,…), incl. contribution to scenario development • ITER System Requirement Document delivered, and Work Breakdown Structure • Integration on ITER, incl. RAMI aspects • DDD2001 conceptual design revised (antenna, T-Lines, control & protection system + assoc. diagnostics, power supply)
Findings • A 20 MW CW LHCD system in ITER is technically feasible, based upon: • - one Passive Active Multijunction (PAM) launcher • N// = 2 (or 1.9) 0.2 • 48 klystrons 500 kW/CW at 5 GHz • (3.7 GHz fall back solution) • 48 main transmission lines (could be halved) • 12 HVPS units (likely 90kV/90A) • Costing: ~ 80M€ (~ 4€/W) • Schedule: 9-10 years, including detailed design and R&D
Passive Active Multijunction Launcher Concept 1152 active waveguides (WG): 48 modules of 6 (poloidal direction) x 4 (toroidal direction) active WGs; One module: 6 rows of multi-junction (24 active WGs), 2 mode converters, 2 tapers, 1 splitter, 1 transmission line, 1 bellow, 1 window [Hillairet, this Conference]
Modification of DDD2001 PAM proposed • 4 active WG modules to improve the flexibility: N// = ± 0.2(initial design: 8-WG module, N// = 2 ± 0.1) • Directivity ~ 70% @ the cut-off density • Optimizing bi-junctions to reduce RC <1.5%, in a wide range of density up to 12 x cut-off density Reflect. coeff. (%) Hillairet, this Conference Milanesio, this Conference
DDD2001 Case B Case A Antenna Front Face • Different models have been analyzed: • DDD2001 PAM model • 2 Alternative PAM models “Case A” and “Case B” • Acceptable Surface Temperature;<650°C for all designs • Better knowledge of the Be-Cu joint (HIP) needed -> R&D required Marfisi, this Conference
B: Transmission lines C: Launcher A: Klystrons ITER LHCD layout • Foreseen distance between the klystrons and the launcher could be reduced at about 50m • 48 rectangular transmision lines maximum (or 24 circular) [Mirizzi this Conference]
LHCD to sustain steady-state long pulses. Its possible mission in ITER Conceptual design of the ITER LHCD system: physics, technology Recent advances of Lower Hybrid Current Drive Technology R&D requirements for ITER Conclusions OUTLINE
High power CW Klystron Development • Toshiba: CW / 5 GHz prototype for KSTAR • Communications and Power Industries, Inc : production in series of CW / 4.6 GHz tubes for EAST (used in C-Mod) • Thalès Electron Devices: production in series(18) CW / 3.7GHz for Tore Supra [Park, Fus. Eng. and Design (2010); Lenci, Vacc. Electronics Conf. IVEC 2009, IEEE International; Kazarian, Fus. Eng. and Design (2009)]
CW high-power tests of the 500kW /5GHz klystron restarted In Feb 2010 at NFRI, with new capability of the test stand. Participation of CEA. 460 kW/20s; ~300kW / CW @ VSWR=1.12 2009 2010
5GHz / CW Klystron Prototype Commissioned at NFRI • So far 300 kW /800s(VSWR = 1.12, efficiency 43%), 460kW/20s (factory test: 300kW/12min; 500kW/0.5s,) Oscilloscope screen shot of the cathode (beam) and the anode voltages and current for 304 kW / 800s pulse [Do, this Conference]
TED 3.7GHz / CW Klystrons for Tore Supra 700 kW / 1000s • 18 klystrons delivered and being commissioned separately • 620kW/CW @ VSWR =1.4routinely, and 720kW/CW @ VSWR=1 • Efficiency of 47% Kazarian et al., FED (2009); Delpech et al., 18th RF Top Conf. (2009)
700kW / CW SPINNER Water Load Validated Delpech this Conference
Manufacturing Tore Supra 3.7GHz PAM launcher Concept. Ph. Bibet Scales as ¼ of the ITER launcher size (7 tons!) Mode Converters (rear view) Passive Active Multijunction (front view) Guilhem, this Conference
An extremely fast commissioning period 2009: 4 days with vacuum conditioning 12 sessions with plasma • 1st discharge with all klystrons: 450kW / 4.5s, N// ok, low reflected power (~1.5%) • 240th plasma pulse: 2.7MW / 17s 2010: • 2.75 MW / 78s (220MJ) • Full current drive during 50s at 2.2MW Participation of 15 collaborators from 7 countries IST, Lisbon; IPP-CR Prague; CCFE, Culham; ENEA-Frascati; IPR, India; SWIP, China; NFRI, South Korea; Ekedahl, to appear in Nucl. Fus. Oct 10
ELHCD = 220MJ ITER-relevant power density for 78s • 2.75MW (25MW/m2) coupled with PAM for 78 seconds • Low reflect. coefficient < 2% at large plasma-launcher gap (density above cut-off) • Efficient cooling: Waveguides/side protections temp. < 300C Infrared monitoring
LHCD Power coupled in ELM-like edge plasmas • Reflection coefficient behaves according to modeling. • Intermediate power (1.5MW) sustained during Supersonic Molecular Beam Injection (SMBI). • No change in Hard X-ray emission profile SMBI is used to mimic ELMs Sharma 37th EPS Conf.
Full Current Drive for 50s • CD efficiency: LHCD ~ 0.8x1019A/W/m2; similar to full active multijunction launchers
LHCD to sustain steady-state long pulses its possible mission in ITER Conceptual design of the ITER LHCD system: physics, technology Recent advances of Lower Hybrid Current Drive Technology R&D requirements for ITER Conclusions OUTLINE
Specific R&D activity • Transmission lines, RF windows, mode filters; must be adapted to ITER constraints • Minimize the number of transmission lines. • 500kW/CW RF windows exposed to the ITER environment must be developed and tested. • PAM plasma facing front • The 500kW/5GHz Toshiba prototype klystron has to be validated @ 500kW/CW under VSWR > 1.4. • Need R&D program, conducted jointly by fusion community and industrial partners, to avoid the risk of failure of fabrication and the excessive cost as well.
CONCLUSIONS • LHCD is a mature method used in a large number of tokamaks • In ITER, LHCD is seen to be a unique CD tool for driving far off-axis current (r/a > 0.6) • An ITER LH voluntary program is underway • A 20 MW / 5 GHz / CW LHCD system using one Passive Active Multijunction (PAM) launcher in ITER is technically feasible • ~ 9 years are necessary between the decision point by stakeholders and the start of the commissioning phase on ITER,if the required R&D is timely initiated and if the competence of Fusion laboratories and industries is maintained