@inproceedings{oai:jaxa.repo.nii.ac.jp:00038819,
 author = {松本, 康司 and 高田, 仁志 and 吉田, 誠 and 東, 伸幸 and 高橋, 綾香 and Matsumoto, Koji and Takada, Satoshi and Yoshida, Makoto and Azuma, Nobuyuki and Takahashi, Ayaka},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島, To achieve light-weight and controllable rocket engine, application of electric control valves has been considered. Since the operating condition and atmosphere of these valves depend on the part of the engine, evaluations of the valves operation in various environments are required. As the operating environment, low and high temperature, vacuum and nitrogen gas conditions are assumed. In this study, to achieve reliable movement of these valves, wear life of the different solid lubricant films expected to apply for the valves were evaluated with different temperature in vacuum condition., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600088000, レポート番号: JSASS-2015-4019},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {大型ロケットエンジン電動バルブ駆動用固体潤滑被膜の評価},
 year = {2015}
}