| タイトル | HAN/HN-Based Monopropellant Thrusters |
| 著者（日） | 福地, 亜宝郎; 長瀬, 栄; 丸泉, 春樹; 綾部統夫 |
| 著者（英） | Fukuchi, Aporo; Nagase, Sakae; Maruizumi, Haruki; Ayabe, Muneo |
| 著者所属（日） | IHIエアロスペース; IHI契約法務部契約グループ; IHIエアロスペース・エンジニアリング; IHI技術開発本部 |
| 著者所属（英） | Technologies Development Department, IHI Aerospace; Contracts Group, Contracts & Leagal Division, IHI; IHI Aerospace Engineering; Corporate Research & Developmet\ntIHI |
| 発行日 | 2010-03-31 |
| 発行機関など | Administration Department, Corporate Research & Development, IHI
IHI技術開発本部管理部 |
| 刊行物名 | IHI Engineering Review |
| 巻 | 43 |
| 号 | 1 |
| 開始ページ | 22 |
| 終了ページ | 28 |
| 刊行年月日 | 2010-03-31 |
| 言語 | eng |
| 抄録 | HAN-based monopropellant has been anticlpated to be an alternative to hydrazine currently used for space propulsion application. They are very favorable in potentially higher performance, significantly less toxic, and environmentally harmless compared with hydrazine. The practical use of HAN-based monopropellant has not been achieved so far due to the lack of reliable ignltion technology with Ir catalysts and because of its complicated combustion mechanism and its high detonability. This paper presents the development and hot firing test results of a mixture of HAN/HN/TEAN/H20. The HN addition realized a reliable catalytic ignition and combustion characteristics with 1 N-20N class thrusters and safety characteristics without detonability. |
| 内容記述 | Original contains color illustrations
形態: カラー図版あり |
| 資料種別 | Article |
| ISSN | 0018-9820 |
| NCID | AA00668470 |
| SHI-NO | AA0064613004 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/15604 |
