2003年
アノードレイヤ型ホールスラスタの作動特性
日本航空宇宙学会誌和文論文論文集
- ,
- ,
- ,
- 巻
- 51
- 号
- 596
- 開始ページ
- 492
- 終了ページ
- 497
- 記述言語
- 日本語
- 掲載種別
- DOI
- 10.2322/jjsass.51.492
- 出版者・発行元
- 日本航空宇宙学会
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 the 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.
- リンク情報
- ID情報
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- DOI : 10.2322/jjsass.51.492
- ISSN : 1344-6460
- CiNii Articles ID : 10011725882
- CiNii Books ID : AA11307372