@inproceedings{oai:jaxa.repo.nii.ac.jp:00014464,
 author = {前田, 真克 and 矢部, 高宏 and 宮崎, 芳郎 and Maeda, Masakatsu and Yabe, Takahiro and Miyazaki, Yoshiro},
 book = {宇宙航行の力学シンポジウム, Symposium on Flight Mechanics and Astrodynamics},
 month = {Dec},
 note = {宇宙航行の力学シンポジウム(平成20年度)(2008年12月4～5日、宇宙航空研究開発機構宇宙科学研究本部), Symposium on Flight Mechanics and Astrodynamics 2008 (December 4-5, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, Because of the high heat rejection demand with advancement of the satellite system, development of a thin heat transport device is needed. We noted oscillating heat pipe with check valves, and made the 3-milimeter-thick prototype. This paper describes the result of performance evaluation test of this prototype., 資料番号: AA0064729041},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {逆止弁付振動流型ヒートパイプの性能評価試験},
 volume = {平成20年度},
 year = {2009}
}