Published November 2013 | Version v1
Journal article

Design of off-midplane launcher (LH3) based on velocity space synergy for Alcator C-Mod

  • 1. Plasma Science Fusion Center, MIT, Cambridge, MA (United States)

Description

A new LH launcher (LH3) is designed for Alcator C-Mod to increase the net LHCD power to 2 MW. With the existing launcher (LH2), LH3 aims to enhance the single pass power absorption to improve LHCD efficiency at high density. For this purpose, launcher design parameters are surveyed to maximize the synergistic effect between LH2. Ray-tracing is extensively used and the launcher location and the launched N = c/v are optimized. At the line averaged density of 1.4x1020 m3, it is predicted that the combination of two launchers can reduce the parasitic edge loss dramatically, and therefore can increase the LH driven current by about 50 - 60% compared to cases in which two launchers are used separately. Based on the parameter survey, an off-midplane launcher (LH3) is designed to be located 15 cm above mid-plane. LH3 employs 8-way power splitters to improve the antenna-plasma coupling. The antenna-plasma coupling simulation is performed using COMSOL and ALOHA codes, predicting 90% of RF power coupling when the launcher front density is high enough (≥ ncutoff). (author)

Availability note (English)

Available from http://dx.doi.org/10.1585/pfr.8.2402143

Additional details

Identifiers

Publishing Information

Journal Title
Plasma and Fusion Research
Journal Volume
8
Journal Issue
special issue 1
Journal Page Range
p. 2402143.1-2402143.5
ISSN
1880-6821

Conference

Title
22. international Toki conference on cross-validation of experiment and modeling for fusion and astrophysical plasmas
Acronym
ITC22
Dates
19-22 Dec 2012
Place
Toki, Gifu (Japan)

INIS

Country of Publication
Japan
Country of Input or Organization
Japan
INIS RN
46134707
Subject category
S70: PLASMA PHYSICS AND FUSION TECHNOLOGY;
Resource subtype / Literary indicator
Conference
Descriptors DEI
ALCATOR DEVICE; AUGMENTATION; EFFICIENCY; HYBRID SYSTEMS; LAUNCHING; LOWER HYBRID CURRENT DRIVE; MODIFICATIONS; PHASE SPACE; PHASE VELOCITY
Descriptors DEC
CLOSED PLASMA DEVICES; MATHEMATICAL SPACE; NON-INDUCTIVE CURRENT DRIVE; SPACE; THERMONUCLEAR DEVICES; TOKAMAK DEVICES; VELOCITY

Optional Information

Notes
24 refs., 6 figs.