JAXA Repository / AIREX 未来へ続く、宙(そら)への英知

このアイテムに関連するファイルはありません。

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
DOIinfo: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
67
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
ISSN1344-6460
ISSN(online)2432-3691
NCIDAA11307372
SHI-NOAA1940218004
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/938022


このリポジトリに保管されているアイテムは、他に指定されている場合を除き、著作権により保護されています。