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In vessel characterization and first power tests on plasma of the Real-Time controllable EC launcher on FTU Tokamak

Authors :
O. D'Arcangelo
S. Garavaglia
V. Muzzini
Luca Boncagni
V. Mellera
Alessandro Bruschi
Giovanni Grosso
Daniela Farina
G. Ramogida
G. Artaserse
Alessandro Simonetto
Gustavo Granucci
S. Cirant
A. Moro
D. Minelli
Carlo Sozzi
Lorenzo Figini
William Bin
C. Galperti
Gabriele D'Antona
Mohsen Davoudi
S. Nowak
Roberto Ferrero
E. Alessi
A. Nardone
Source :
EPJ Web of Conferences, Vol 32, p 02018 (2012), EC-17, 17th Joint Workshop on Electron Cyclotron Emission and Electron Cyclotron Resonance Heating, Deurne-The Netherlands, May 7-10, 2012, info:cnr-pdr/source/autori:Moro A.; Alessi E.; Artaserse G.; Bin W.; Boncagni L.; Bruschi A.; Cirant S.; D'Antona G.; D'Arcangelo O.; Davoudi M.; Farina D.; Ferrero R.; Figini L.; Galperti C.; Garavaglia S.; Granucci G.; Grosso G.; Mellera V.; Minelli D.; Muzzini V.; Nardone A.; Nowak S.; Ramogida G.; Simonetto A.; and Sozzi C./congresso_nome:EC-17, 17th Joint Workshop on Electron Cyclotron Emission and Electron Cyclotron Resonance Heating/congresso_luogo:Deurne-The Netherlands/congresso_data:May 7-10, 2012/anno:2012/pagina_da:/pagina_a:/intervallo_pagine
Publication Year :
2012
Publisher :
EDP Sciences, 2012.

Abstract

The Electron Cyclotron (EC) fast launcher for real time control experiments has been installed on FTU and characterized to be fully integrated in a real-time MHD control module under development. The launcher scheme is based on a two module sys- tem, symmetric with respect to the equatorial plane of FTU, with a front steering concept and the launched beams are real-time controllable both in poloidal and toroidal directions. Specific design parameters, defined by the FTU MHD dynamics (typically island size and q profile changes), are the beam dimensions with zooming capabilities, the steering range and mirror speed with the most demanding requirement on poloidal speed of the Steering Mirror (SM) = 1 in 10 ms. A set of tests has been done to verify the system perfor- mance. High power tests of the launcher have been done on a 500 kA, 0.5 10 20 m -3 and 5.3 T plasma with 2 300 kW of EC power delivered to the plasma. The steering mechanism was tested under the automatic control system and showed a dynamic response in line with the requirements. Results of these tests will be presented in the paper.

Details

Language :
English
Volume :
32
Database :
OpenAIRE
Journal :
EPJ Web of Conferences
Accession number :
edsair.doi.dedup.....fb6723b236885807d2da9dd608381654