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＜journal article＞
アノードレイヤ型ホールスラスタの作動特性

Creator
Creator Name
山本, 直嗣
Yamamoto, Naoji
ヤマモト, ナオジ
Affiliation
Affiliation Name
東京大学大学院工学系研究科宇宙工学専攻
Creator Name
中川, 貴史
Nakagawa, Takahumi
ナカガワ, タカフミ
Affiliation
Affiliation Name
三菱電機（株） | 東京大学大学院工学系研究科宇宙工学専攻
Creator Name
小紫, 公也
Komurasaki, Kimiya
コムラサキ, キミヤ
Affiliation
Affiliation Name
東京大学大学院新領域創成科学研究科先端エネルギー工学専攻
Creator Name
荒川, 義博
Arakawa, Yoshihiro
アラカワ, ヨシヒロ
Affiliation
Affiliation Name
東京大学大学院工学系研究科宇宙工学専攻
Language
Japanese
Publisher
日本航空宇宙学会
The Japan Society for Aeronautical and Space Sciences(JSASS)
Date
2003-09
Source Title
日本航空宇宙学会論文集
Vol
51
Issue
596
First Page
492
Last Page
497
Publication Type
Accepted Manuscript
Access Rights
open access
Related DOI
日本航空宇宙学会論文集 || 51(596) || p492-497
http://www.jsass.or.jp/web/index.php
Related URI
日本航空宇宙学会論文集 || 51(596) || p492-497
http://www.jsass.or.jp/web/index.php
Relation
日本航空宇宙学会論文集 || 51(596) || p492-497
http://www.jsass.or.jp/web/index.php
Abstract Thrust performance and stable operation conditions of an anode layer type Hall thruster was investigated using a 1.5kW class anode layer type Hall thruster. The thrust efficiency reached at 53% with t...he specific impulse of 2,000s, which are competitive with these of SPT-100 thrusters. Anode shape and axial position of the anode were changed. Stability of the discharge was found sensitive to the anode configuration and applied magnetic flux density.show more

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Details

Record ID
16994
Peer-Reviewed
Refereed
Subject Terms
Electric Propulsion
Hall Thruster
Anode Layer
Hollow Anode
ISSN
1344-6460
NCID
AA11307372
Created Date 2010.04.27
Modified Date 2022.01.24

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