@inproceedings{oai:jaxa.repo.nii.ac.jp:00038605,
 author = {森谷, 信一 and 齋藤, 俊仁 and 竹腰, 正雄 and 橋本, 知之 and 高橋, 正晴 and Moriya, Shinichi and Saito, Toshihito and Takegoshi, Masao and Hashimoto, Tomoyuki and Takahashi, Masaharu},
 book = {第57回宇宙科学技術連合講演会講演集, Proceedings of 57th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第57回宇宙科学技術連合講演会（2013年10月9日-11日. 米子コンベンションセンター（BiG SHiP）), 米子市, 鳥取県, Establishment of a life enhancing design technology for a combustion chamber is strongly required to realize thereusable rocket engine system. The most effective method to prolong the chamber life is to reduce the thermal load to thechamber wall, and applications of a thermal barrier coating and film cooling of a throat region are being investigated inJAXA. On the other hand, a life test using an actual chamber is a very cost and time consuming method. Therefore, theaccelerated test method for evaluation of a chamber life is also investigated., 資料番号: AC1400021000, レポート番号: JSASS-2013-4278},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {LOX/エタノール燃焼器の長寿命化},
 year = {2013}
}