@article{oai:jaxa.repo.nii.ac.jp:00032832,
 author = {橋本, 保成 and 秋葉, 鐐二郎 and 倉谷, 健治 and 小竹, 進 and 藤田, 重実 and Hashimoto, Y. and Akiba, R. and Kuratani, K. and Kotake, S. and Fujita, S.},
 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 porous injector face plate for hydrogen transpiration cooling of 10-ton thrust rocket thrust chamber using LH_2-LOX as propellant has been developed and its gas dynamical aspects have been investigated with experiments. The wire mesh laminate fabricated, consist of 12-layers of 12-64 Dutch weave SUS 316 mesh bonded each other by diausion bonding process under vacuum condition. Characteristics of these face plates are investigated in special reference to the flow rate and the temperature profile under the conditions of transpiration cooling. Data obtained by experiments are compared with the values predicted by existing theories with some extension needed to match the present range of prameters., 資料番号: SA0166601000},
 pages = {269--280},
 title = {10 トン溝構造燃焼器用噴射器面多孔質板の試作研究},
 volume = {6},
 year = {1983}
}