@inproceedings{oai:jaxa.repo.nii.ac.jp:00038771,
 author = {佐藤, 正喜 and 橋本, 知之 and 森谷, 信一 and 木村, 俊哉 and 八木下, 剛 and 高木, 寛之 and 藤井, 拓也 and 佐藤, 克利 and Sato, Masaki and Hashimoto, Tomoyuki and Moriya, Shin-ichi and Kimura, Toshiya and Yagishita, Tsuyoshi and Takagi, Hiroyuki and Fujii, Takuya and Sato, Katsutoshi},
 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, 鹿児島県, The regenerative cooling combustion chamber of a liquid propellant rocket engine is one of the critical components to limit the life of engine. Especially for the reusable rocket engine combustor, it is important to develop an effective nondestructive inspection technique to assure its life. JAXA/ISAS developed a reusable LOX/LH2 rocket engine for the Reusable Sounding Rocket and conducted 142 times of engine firings. In the series of firing tests, 4 times of nondestructive inspection of the combustion chamber was carried out using a high-energy X-ray CT system of Hitachi, Ltd. By making full use of image analysis technique, the deformation of chamber inner wall and the distribution of chamber wall thickness can be evaluated, and their transitional progress due to the repeated engine firing tests are also clarified., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600029000, レポート番号: JSASS-2015-4443},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {高エネルギーX線CTを用いた再使用ロケットエンジン燃焼室の非破壊検査},
 year = {2015}
}