書誌事項
- タイトル別名
-
- Experimental Sensitivity Analysis of Operational Points of the Microwave-discharge Miniature Ion Thruster
- マイクロハ ホウデンシキ コガタ イオンスラスタ ニ オケル サドウテン ノ ジッケンテキ カンド カイセキ
この論文をさがす
説明
<p>The microwave-discharge miniature ion thrusters were installed and demonstrated on HODOYOSHI-4 and PROCYON. The ion thruster on PROCYON had some troubles and its lack of robustness was exposed. In this study, we conducted three ground experiments to reveal the important controlled parameters or external factors on the performance of the ion thruster. The dependence on the controlled parameters, the mass flow rates and the microwave power inputs, was investigated using an ion thruster which was designed as same as the flight model. The effect of two external factors, the structure inference and the temperature, was also tested using the structure and thermal model of PROCYON. As a result, we reported some knowledge which should be considered on the small-satellite development with an ion thruster. </p>
収録刊行物
-
- 日本航空宇宙学会論文集
-
日本航空宇宙学会論文集 67 (3), 74-80, 2019
一般社団法人 日本航空宇宙学会
- Tweet
詳細情報 詳細情報について
-
- CRID
- 1390564238099167872
-
- NII論文ID
- 130007659816
-
- NII書誌ID
- AA11307372
-
- ISSN
- 24323691
- 13446460
-
- NDL書誌ID
- 029781655
-
- 本文言語コード
- ja
-
- データソース種別
-
- JaLC
- NDL
- Crossref
- CiNii Articles
- KAKEN
-
- 抄録ライセンスフラグ
- 使用不可