書誌事項
- タイトル別名
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- Research and Development of the Pulsed Plasma Rocket Engine System onboard Osaka Institute of Technology Micro Artificial Satellite
- オオサカ コウギョウ ダイガク チョウコガタ ジンコウ エイセイ トウサイヨウ パルスプラズマロケットエンジン システム ノ カイハツ ケンキュウ
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説明
The Project of Osaka Institute of Technology Electric-Rocket-Engine onboard Small Space Ship (PROITERES) was started at Osaka Institute of Technology in 2007. In PROITERES, a micro satellite with electrothermal pulsed plasma thrusters (PPTs) will be launched in 2010. The main mission is the first powered flight of micro satellite by electric thruster all over the world. This study aims at improvement in performance by changing configuration of PPTs. The total impulse of about 5 Ns was achieved with a teflon cylindrical discharge chamber 9.0 mm in length and 1.0 mm in diameter in 53,000-shot operation with 2.43 J/shot. Finally, the engineering model of PPT system was developed, and it is under operation as final test.
収録刊行物
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- 電気学会論文誌． Ａ
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電気学会論文誌． Ａ 130 (10), 851-857, 2010
一般社団法人 電気学会
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詳細情報 詳細情報について
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- CRID
- 1390282679575613952
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- NII論文ID
- 10026693165
- 130000415278
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- NII書誌ID
- AN10136312
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- ISSN
- 13475533
- 03854205
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- NDL書誌ID
- 10830582
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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
