| タイトル | 全天X線監視装置 (MAXI) 搭載ループヒートパイプ |
| その他のタイトル | Loop Heat Pipe and Radiator System (LHPRS) onboard Monitor of All-sky X-ray Image (MAXI) |
| 参考URL | http://www.jasma.info/journal/?journal-cat=journal |
| 著者（日） | 上野, 史郎 |
| 著者（英） | Ueno, Shiro |
| 著者所属（日） | 宇宙航空研究開発機構宇宙科学研究所ＩＳＳ科学プロジェクト室(JAXA)(ISAS) |
| 著者所属（英） | ISS Science Project Office, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) |
| 発行日 | 2011 |
| 発行機関など | 日本マイクログラビティ応用学会
Japan Society of Microgravity Application |
| 刊行物名 | 日本マイクログラビティ応用学会誌
JASMA : Journal of the Japan Society of Microgravity Application |
| 巻 | 28 |
| 号 | 1 |
| 開始ページ | 34 |
| 終了ページ | 41 |
| 刊行年月日 | 2011 |
| 言語 | jpn
eng |
| 抄録 | This report presents an introduction to loop heat pipes (LHP). Fundamental characteristics of LHP are described in comparison with conventional heat pipes. Following a brief explanation of the operating principle of LHP, the focus is placed on a unique implementation of LHP, the MAXI loop heat pipe radiator system (LHPRS). Since August 2009, LHPRS is working as the heat transporting system to reject heat from the X-ray CCD camera (SSC) of Monitor of All-sky X-ray Image (MAXI) onboard the International Space Station. LHPRS has two separate radiators operating under transient thermal conditions. A brief examination of the flight data shows no performance degradation of LHPRS. The importance of subcooling is stressed for understanding the working principle of the startup and shut-off heaters of LHPRS. This report may be useful for potential LHP users. |
| 内容記述 | 形態: 図版あり
Physical characteristics: Original contains illustrations |
| 資料種別 | Journal Article |
| NASA分類 | Fluid Mechanics and Thermodynamics |
| ISSN | 0915-3616 |
| NCID | AN10537663 |
| SHI-NO | AA1440124000 |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/18671 |
