タイトル | 磁束ピンニング効果を用いた非接触微小擾乱抑制機構のための基礎特性評価 |
その他のタイトル | Performance Evaluation for a Contactless Micro Vibration Isolator Using the Flux Pinning Effect |
DOI | info:doi/10.2322/jjsass.67.126 |
著者(日) | 柴田, 拓馬; 坂井, 真一郎 |
著者(英) | Shibata, Takuma; Sakai, Shinichiro |
著者所属(日) | 総合研究大学院大学(SOKENDAI); 総合研究大学院大学(SOKENDAI) : 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) |
著者所属(英) | The Graduate University for Advanced Studies (SOKENDAI); The Graduate University for Advanced Studies (SOKENDAI) : Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) |
発行日 | 2019-08-05 |
発行機関など | 日本航空宇宙学会 Japan Society for Aeronautical and Space Sciences |
刊行物名 | 日本航空宇宙学会論文集 Journal of the Japan Society for Aeronautical and Space Sciences |
巻 | 67 |
号 | 4 |
開始ページ | 126(24) |
終了ページ | 135(33) |
刊行年月日 | 2019-08-05 |
言語 | jpn eng |
抄録 | Micro vibrations and heat generated by reaction wheels and a refrigerator cause a problem in observing stars or galaxies with high pointing accuracy. Several methods have been proposed for reducing the influence of the vibration. However, these methods are difficult to cut low frequency band off passively. In addition, thermal strain on a primary mirror decreases the pointing accuracy when the heat transmits to a mission part through conventional vibration isolator. A vibration isolator using the flux pinning effect is proposed for solving the problem in this paper. The pinning force can maintain the relative distance and attitude between a type-II superconductor and a magnet without control. The spring and damping characteristics of the pinning force is applied to suppress the vibration effect. A mission part and bus part is not connected mechanically but electromagnetically, therefore it is expected that the influence of the heat transfer can decrease. Results of numerical analysis and experiment are given for discussing the feasibility of the proposed mechanism. |
内容記述 | 形態: 図版あり Physical characteristics: Original contains illustrations |
キーワード | Micro Vibration Isolator; Flux Pinning Effect; Formation Flying |
資料種別 | Journal Article |
NASA分類 | Spacecraft Design, Testing and Performance |
ISSN | 1344-6460 |
ISSN(online) | 2432-3691 |
NCID | AA11307372 |
SHI-NO | AA1940218004 |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/938022 |