Výsledky vyhledávání - "Uchimi, Masaharu"

Autor: Nakata, Daisuke, Minato, Ryojiro, Yoshikawa, Inaho, Yagihashi, Hiromitsu, Arimatsu, Koki, Uchimi, Masaharu

Publikováno v: 平成30年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2018.

平成30年度宇宙輸送シンポジウム（2019年1月17日-18日. 宇宙航空研究開発機構宇宙科学研究所（JAXA)(ISAS)）, 相模原市, 神奈川県
Space Transportation Symposium FY2018 (January 17-18, 2019. Institute of Spac

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::c1997072843bd9620681b7a8aa49aedf
http://id.nii.ac.jp/1696/00015333/

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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

Autor: Takida, Junya, Fukuoka, Masaru, Kunieda, Maro, Funazaki, Kenichi, Uchimi, Masaharu

Publikováno v: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum. :1-9

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 specificati

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9911596f618d091373e1544d16de3264
http://id.nii.ac.jp/1696/00002528/

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Optimal Design of Internal Flow System in Rocket Pump Considering Axial Dynamic Characteristics

Autor: Kawasaki, Satoshi, Shimura, Takashi, Uchimi, Masaharu, Hayashi, Mitsuhiro, Matsui, Jun

Publikováno v: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum. :1-8

In a rocket turbopump, an axial thrust balancing system with the balance piston is often applied to reduce the axial thrust. The leakage flow through the balance piston is affected by the configuration of the balance piston and the balancing point in

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::9a32614c85ae9e7efcb6a2187e82cf80
http://id.nii.ac.jp/1696/00002532/

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Reduction in Thomas Force of Rocket Turbopump Turbine by Using Robust Design Process

Autor: Takida, Junya, Uchimi, Masaharu, Shimagaki, Mitsuru, Funazaki, Kenichi

Publikováno v: 宇宙航空研究開発機構研究開発資料 = JAXA Research and Development Memorandum. :1-7

An application of robust design process for reduction in Thomas force of rocket turbopump turbines is presented in this paper．Because of its special specification, rocket turbopump turbines are designed as supersonic impulse turbines, and as a resu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=jairo_______::888abc7aeeb3fbdb9918a85a3a5b77d1
http://id.nii.ac.jp/1696/00002538/

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