@techreport{oai:jaxa.repo.nii.ac.jp:00002534,
 author = {瀧田, 純也 and 福岡, 勝 and 國枝, 麿 and 船崎, 健一 and 内海, 政春 and Takida, Junya and Fukuoka, Masaru and Kunieda, Maro and Funazaki, Kenichi and Uchimi, Masaharu},
 month = {Mar},
 note = {An application of QFD (Quality Function Deployment) method for the design of rocket turbopump turbines is presented in this paper. Generally rocket turbopump turbines are designed as supersonic impulse turbines, and because of its special specifications, improvements on turbine efficiency and robustness is difficult. Further improvement on turbine design techniques is needed, because turbine performance directly affects engine performance and reliability in a liquid rocket propulsion system. The purpose of present work is to improve turbine design techniques by applying QFD method to the rocket turbopump turbines. In this presentation,  the QFD results for the identification of important design parameters and for the visualization of the market needs which was obtained from rocket engine stakeholders are discussed., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA0065218000, レポート番号: JAXA-RM-11-021},
 title = {QFD を用いたロケットターボポンプ用タービンの重要設計パラメータの抽出},
 year = {2012}
}