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直流アークジェットスラスタの低毒性推薬分解ガス適合性に関する研究
https://jaxa.repo.nii.ac.jp/records/16690
https://jaxa.repo.nii.ac.jp/records/16690dd659dac-7b8f-47f1-a6c9-452d3249f9af
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 直流アークジェットスラスタの低毒性推薬分解ガス適合性に関する研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | DC Arcjet Thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hydroxyl Ammonium Nitrate (HAN) | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hydrazine | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Compatibility Study of Low Toxicity Propellant Decomposed Gas for Direct Current Arcjet Thruster | |||||
著者 |
岡町, 悠介
× 岡町, 悠介× 中川, 定紀× 田原, 弘一× 長田, 泰一× 増田, 井出夫× Okamachi, Yusuke× Nakagawa, Sadanori× Tahara, Hirokazu× Nagata, Taiichi× Masuda, Ideo |
|||||
著者所属 | ||||||
大阪工業大学 | ||||||
著者所属 | ||||||
大阪工業大学 | ||||||
著者所属 | ||||||
大阪工業大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成21年度, 発行日 2010-01 |
|||||
会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Hydrazine is used as a propellant of spacecraft thruster. However, hydrazine is a high toxicity liquid. Spacecraft researchers need a low toxicity propellant. Hydroxyl Ammonium Nitrate (HAN: NH3OHNO3) is proposed as low toxicity propellant. The propellant causes the severe chemical reaction, and the electrode is consumed for electic thrusters. In this study, the capability of HAN for DC Arcjet Thruster's propellant is examined. As a result, although the erosion rate of the electrode was severe, after improvement the long-time operation was achieved. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064741120 |