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- KOJIMA Kohei
- Mitsubishi Heavy Industries, Ltd.
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- YOKOTA Shigeru
- University of Tsukuba
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- YAMASAKI Junko
- University of Tsukuba
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- YONAHA Moyuru
- University of Tsukuba
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- KIMURA Tatsuya
- Mitsubishi Heavy Industries, Ltd.
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- KAWAMATA Yoshihiro
- Mitsubishi Heavy Industries, Ltd.
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- YASUI Masaaki
- Mitsubishi Heavy Industries, Ltd.
説明
<p>In recent years, high power electric propulsion systems in the range of several tens to 100 kW are under development for the cargo of the manned missions or the satellite market. The thrusters for these propulsion systems require around 100 A of the discharge current. For these applications, we have been developing a 100 A class hollow cathode. To appropriate the electron emission processes of the LaB6 insert in a 100 A class Hollow Cathode, the characteristics and the diagnostics by single Langmuir probing were investigated. In this paper we report the results and the guidelines for the next step in a 100 A class heaterless hollow cathode.</p>
収録刊行物
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- TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN
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TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN 17 (1), 90-95, 2019
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
- 1390845713037573248
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- NII論文ID
- 130007542875
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- ISSN
- 18840485
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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
- KAKEN
- OpenAIRE
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- 抄録ライセンスフラグ
- 使用不可