@inproceedings{oai:jaxa.repo.nii.ac.jp:00038606,
 author = {竹腰, 正雄 and 齋藤, 俊仁 and 小野, 文衛 and 森谷, 信一 and Takegoshi, Masao and Saito, Toshihito and Ono, Fumiei and Moriya, Shinichi},
 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, The film cooling effectiveness on ethanol were acquired with a rocket thrust chamber. The length of the liquid phase filmcooling Lc was evaluated experimentally. The calculated Lc was a good agreement with that obtained by the combustiontests. The techniques of film cooling for the long life and the reusable rocket thrust chamber were also discussed in thisstudy., 資料番号: AC1400022000, レポート番号: JSASS-2013-4279},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences(JSASS)},
 title = {ロケット燃焼器におけるエタノールフィルム冷却の効果と燃焼器の長寿命化},
 year = {2013}
}