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Vacuum Insulation and Achievement of 980 keV,185 A/m^2 H-Ion Beam Acceleration at JAEA for the ITER Neutral Beam Injector

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Plasma Science and Technology 2013年第2期15卷 179-183页

作者： Hiroyuki TOBARI Masaki TANIGUCHI Mieko KASHIWAGI Masayuki DAIRAKU Naotaka UMEDA Haruhiko YAMANAKA Kazuki TSUCHIDA Jumpei TAKEMOTO Kazuhiro WATANABE Takashi INOUE keishi sakamoto Japan Atomic Energy Agency (JAEA) Mukouyama 801-1 Naka Ibaraki 311-1093 Japan

Abstract Vacuum insulation of -1 MV is a common issue for the HV bushing and the accel- erator for the ITER neutral beam injector （NBI）. The HV bushing as an insulating feedthrough has a five-stage structure and each stage consists of double-layered insulators. To sustain -1 MV in vacuum, reduction of electric field at several triple points existing around the double-layered insulators is a critical issue. To reduce electric field simultaneously at these points, three types of stress ring have been developed. In a voltage holding test of a full-scale mockup equipped with these stress rings, 120% of rated voltage was sustained and the voltage holding capability required in ITER was verified. In the MeV accelerator, whose target is the acceleration of a H- ion beam of 1 MeV, 200 A/mS, the gap between the grid support was extended to suppress breakdowns triggered by electric field concentration at the edge and corner of the grid support. This modi- fication improved the voltage holding capability in vacuum, and the MeV accelerator succeeded in sustaining -1 MV stably, b-~rthermore, it appeared that the H- ions beam was deflected and a part of the beam was intercepted at the acceleration grid, This causes high heat load on the grids and breakdowns during beam acceleration. To suppress the direct interception, a new grid was designed with proper aperture displacement based on a three dimensional beam trajectory analysis, As a result, 980 keV, 185 A/ms H- ion beam acceleration has been demonstrated, which is close to the ITER requirement.

关键词： neutral beam injector (NBI) negative ion beam HV bushing vacuum insu-lation

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Rocket Propulsion Powered Using a Gyrotron

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Journal of Energy and Power Engineering 2017年第6期11卷 363-371页

作者： Masafumi Fukunari Kimiya Komurasaki Yusuke Nakamura Yasuhisa Oda keishi sakamoto Research Center for Development of Far-Infrared Region University of Fukui Fukui 910-8507 Japan Department of Aeronautics & Astronautics University of Tokyo Bunkyo Tokyo 113-8656 Japan Graduate School of Frontier Sciences University of Tokyo Kashiwa Chiba 277-8561 Japan National Institutes for Quantum and Radiological Science and Technology Naka Ibaraki 311-0193 Japan

Abstract： This paper presents a review of a beamed energy propulsion rocket, the Microwave Rocket, WlllCn proauces propmslve thrust from millimeter-wave beams transferred from the ground. The thrust is generated through millimeter-wave discharge driven in a cylindrical thruster. As a high-power millimeter-wave generator, a Gyrotron is promising as the beam source. The salient benefit of Microwave Rockets is the resultant drastic cost reduction of mass transportation into space. We have already conducted launch experiments and have achieved continuous thrust generation under multi-pulse operation. Recently, a long-distance beam transfer system has been developed. Ignition tests have been conducted. The physics of the millimeter-wave discharge remain unclear. Additional studies using exoerimentation and calculations must be conducted to optimize the thrust generation.

关键词： Beamed energy propulsion microwave discharge wireless power transfer gyrotron.

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