書誌事項
- タイトル別名
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- Development of a Space Plasma Simulator Using an Electron Cyclotron Resonance Plasma Accelerator.
- デンシ サイクロトロン キョウメイ ホウデンガタ プラズマ カソクキ オ モチ
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抄録
A ground facility was developed for simulation of material and space plasma interaction and for study of spacecraft charging and discharge phenomena. The space plasma simulator consisted of a vacuum tank 0.7m in diameter ×1.5m long, two turbo-molecular pumps with pumping speeds 5 and 3m3/s, respectively, achieving some 10-4Pa, and an electron cyclotron resonance plasma source of a magnetic-field-expansion plasma accelerator. Oxygen or nitrogen plasma properties of plasma density, electron temperature, ion incident energy, ion freestream velocity and atomic oxygen flux were measured. The simulator was found to have a high potential for ground tests.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 45 (522), 396-403, 1997
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
- 1390282679455281536
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- NII論文ID
- 10002861804
- 10004209428
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
- http://id.crossref.org/issn/00214663
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- NDL書誌ID
- 4257410
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可