@article{oai:jaxa.repo.nii.ac.jp:00032830,
 author = {秋葉, 鐐二郎 and 堀内, 良 and 倉谷, 健治 and 高野, 雅弘 and 斉藤, 敏 and 橋本, 保成 and 成尾, 芳博 and 湯沢, 克宣 and 松原, 十四生 and Akiba, Ryojiro and Horiuchi, Ryo and Kuratani, Kenji and Kohno, Masahiro and Saito, S. and Hashimoto, Yasunari and Naruo, Yoshihiro and Yuzawa, K. and Matsubara, T.},
 journal = {宇宙科学研究所報告. 特集: 液水/液酸エンジンの開発研究報告},
 month = {Mar},
 note = {A 10-ton thrust rocket engine thrust chamber made by diffusion melt bonding processes was successfully demonstrated. The regeneratively cooled thrust chamber has been designed, fabricated and tested. This chamber consists of an inner OFHC copper liner which was milled by machining process and bonded with SUS316L outer shell by means of diffusion bonding with thin Ag layer. The Ag layer was superposed on a Ni layer which plated on the inner surface of outer shell split into two sections. The demonstration tests were conducted at a chamber pressure of about 30 kgf/cm^2a and an oxidant-fuel ratio of 6.0 using hydrogen-oxygen as propellant. Data obtained in several static-firing tests are discussed and analyzed., 資料番号: SA0166599000},
 pages = {229--257},
 title = {液水/液酸 10 トン溝構造燃焼器の試作と燃焼実験},
 volume = {6},
 year = {1983}
}