Zobrazeno 1 - 10
of 118
pro vyhledávání: '"Ishikawa Yasuhiro"'
Autor:
YAGISHITA, Tsuyoshi, TAKESAKI, Yuichiro, IRIKADO, Tomoko, KAGA, Toru, KOBAYASHI, Hiroaki, MORI, Hatsuo, ISHIKAWA, Yasuhiro
Publikováno v:
令和4年度宇宙輸送シンポジウム: 講演集録 = Proceedings of Space Transportation Symposium FY2022.
令和4年度宇宙輸送シンポジウム（2023年1月12日-13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 FY2022 (January 12-13, 2023. Institute of Space
Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::1d31c935759eb594c3ee2efa4bc8bc3c
http://id.nii.ac.jp/1696/00049470/
http://id.nii.ac.jp/1696/00049470/
Autor:
Horigome, Hitoshi1, Ishikawa, Yasuhiro2 wavelet@nifty.ne.jp, Takahashi, Kazuhiro3, Yoshinaga, Masao4, Sumitomo, Naokata5
Publikováno v:
Scientific Reports. 6/7/2021, Vol. 11 Issue 1, p1-12. 12p.
Publikováno v:
In Journal of Materials Research and Technology July-September 2012 1(2):96-102
Publikováno v:
In Colloids and Surfaces B: Biointerfaces 2005 46(3):147-151
Publikováno v:
In Colloids and Surfaces B: Biointerfaces 2005 45(1):35-41
Publikováno v:
In Colloids and Surfaces B: Biointerfaces 2005 42(1):53-58
JAXA and IHI have been conducting research to develop a high performance methane rocket engine such as specific impulse (Isp) of 370 secs, and a multi-element injector and a regeneratively cooled combustion chamber were designed. This study conducts
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::06de72b451f7c259c3d0f41bd4438b53
Autor:
Horigome, Hitoshi1, Ishikawa, Yasuhiro2 wavelet@nifty.ne.jp, Takahashi, Kazuhiro3, Yoshinaga, Masao4, Sumitomo, Naokata5
Publikováno v:
Scientific Reports. 8/19/2021, Vol. 11 Issue 1, p1-2. 2p.
Akademický článek
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Autor:
KATO, Toshiki, TERAKADO, Daiki, NANRI, Hideaki, MORITO, Toshiki, MASUDA, Ideo, ASAKAWA, Hiroya, SAKAGUCHI, Hiroyuki, ISHIKAWA, Yasuhiro, INOUE, Takuma, ISHIHARA, Shinji, SASAKI, Masahiro
JAXA and IHI have been proceeding the research and development activities for high performance LOX/Methane regenerative cooling engine since 2013. It is targeted that the specific impulse of 370 sec will be achieved due to the high combustion efficie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a6474630e885cbb66c8e406cfa2a0483