Diagnostics of Xe Ion in an Anode-layer Type Hall Thruster Using Laser-Induced Fluorescence
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- YOKOTA Shigeru
- Department of Aeronautics and Astronautics, The University of Tokyo
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- LEMPKE Markus
- Institute of Space Systems, University of Stuttgart
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- MATSUI Makoto
- Department of Aeronautics and Astronautics, The University of Tokyo
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- HARA Kentaro
- Department of Aeronautics and Astronautics, The University of Tokyo
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- KOMURASAKI Kimiya
- Department of Aeronautics and Astronautics, The University of Tokyo
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- ARAKAWA Yoshihiro
- Department of Aeronautics and Astronautics, The University of Tokyo
抄録
The discharge oscillation in an anode-layer type Hall thruster is one of the most serious problems to be overcome. In general, a hollow anode is used in order to stabilize the operation. Recent numerical simulation results show the stable operation depends on the ionization rate in the hollow anode. In order to verify the simulation result, it is needed to measure the plasma profile in the hollow anode.<br>In this paper, as a first step, the number density and the velocity distribution of single-charged xenon ions in an anode-layer type Hall thruster were investigated by means of Laser-Induced Fluorescence (LIF) for the 5d2F7/2→6p2D05/2 excitation transition at 834.7 nm detecting the non-resonant line to the 6s2P3/2 state at 541.9 nm. As a result, we obtained the relative ion number density and the velocity distributions. The ion velocity distribution function shows both ionization and acceleration occur in the acceleration channel, while only ionization occurs in the hollow anode.
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, SPACE TECHNOLOGY JAPAN 7 (ists26), Pb_131-Pb_134, 2009
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390282680188854016
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- NII論文ID
- 130000151972
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- ISSN
- 13473840
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- 本文言語コード
- en
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可