Zobrazeno 1 - 10
of 16
pro vyhledávání: '"Asakawa, Hiroya"'
This paper describes the design and the experimental result of the cryogenic propellant valves which are actuated by the electric motor. Through three years of a development term, the valve experienced several elemental tests to investigate its chara
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::75e2440d7847d4125c5c69369dfee1a8
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
Autor:
ASAKAWA, Hiroya, SAKAGUCHI, Hiroyuki, MORI, Hatsuo, KATO, Toshiki, NANRI, Hideaki, MORITO, Toshiki, MASUDA, Ideo
For small thrust LOX/methane rocket engine, new cryogenic propellant valves which are actuated by an electric motor were developed. The valves have the functions not only for the shut-off valves, but also the control of the propellant flow rate. Sinc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d735e6ee883960a49632e38ca7b0cf3a
Akademický článek
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Autor:
Oniduka, Hisakazu, Kano, Yasuhito, Ishihara, Shinji, Inoue, Takuma, Masuda, Ideo, Asakawa, Hiroya, Tomita, Takeo, Sasaki, Masaki, Onodera, Takuo, Nunome, Yoshio
Publikováno v:
第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム.
第47回流体力学講演会/第33回航空宇宙数値シミュレーション技術シンポジウム (2015年7月2日-3日. 東京大学), 目黒区, 東京
47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (J
47th Fluid Dynamics Conference /the 33rd Aerospace Numerical Simulation Symposium (J
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::ea8f9821e392d36e031528af5b281456
http://id.nii.ac.jp/1696/00038789/
http://id.nii.ac.jp/1696/00038789/
Autor:
Nakasuka, Shinichi, Makino, Takashi, Amimoto, Junichi, Fukunaga, Mihoko, Asakawa, Hiroya, Tanaka, Nohiro, Tsurui, Y., Okubo, Takuya
Publikováno v:
大気球シンポジウム: 平成21年度 = Balloon Symposium: 2009. :100-103
大気球シンポジウム 平成21年度 (2009年10月1-2日. 宇宙航空研究開発機構宇宙科学研究本部), 相模原, 神奈川
Balloon Symposium 2008 (October 1-2, 2009. Institute of Space and Astronautical Science, Japan Aerospac
Balloon Symposium 2008 (October 1-2, 2009. Institute of Space and Astronautical Science, Japan Aerospac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::a517ea34bf89b71ab0f12c645ffe913e
http://id.nii.ac.jp/1696/00018732/
http://id.nii.ac.jp/1696/00018732/
Autor:
Ishihara, Shinji, Inoue, Takuma, Ishizaki, Shinichiro, Masuda, Ideo, Asakawa, Hiroya, Tomita, Takeo, Sasaki, Masaki, Onodera, Takuo, Nunome, Yoshio
Publikováno v:
第59回宇宙科学技術連合講演会講演集 = Proceedings of 59th Space Sciences and Technology Conference.
第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島県
JAXA, IHI, and IA are studying LOX/Methane rocket engine with the regenerative cooled combustion chamber. This p
JAXA, IHI, and IA are studying LOX/Methane rocket engine with the regenerative cooled combustion chamber. This p
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::645133fcf75972904efcc8d8ec164015
http://id.nii.ac.jp/1696/00038748/
http://id.nii.ac.jp/1696/00038748/
Autor:
Asakawa, Hiroya, Nanri, Hideaki, Masuda, Ideo, Ishimoto, Shinji, Inoue, Takuma, Ishihara, Shinji, Ishizaki, Shinichiro, Yonemoto, Koichi
Publikováno v:
第59回宇宙科学技術連合講演会講演集 = Proceedings of 59th Space Sciences and Technology Conference.
第59回宇宙科学技術連合講演会（2015年10月7日-14日. かごしま県民交流センター), 鹿児島市, 鹿児島
This paper reports the result of conceptual study on LOX/LNG(methane) engine for WIRES#015 (WInged Reusable Soundi
This paper reports the result of conceptual study on LOX/LNG(methane) engine for WIRES#015 (WInged Reusable Soundi
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0b7c5a3ef6eb8f11e86a92d2c51204c5
http://id.nii.ac.jp/1696/00038800/
http://id.nii.ac.jp/1696/00038800/
Autor:
Masuda, Ideo, Asakawa, Hiroya, Kubota, Isao, Umemura, Yutaka, Sasagawa, Chiharu, Ishikawa, Yasuhiro, Shinohara, Ryu
Publikováno v:
第59回宇宙科学技術連合講演会講演集 = Proceedings of 59th Space Sciences and Technology Conference.
第59回宇宙科学技術連合講演会（2015年10月7日-15日. かごしま県民交流センター), 鹿児島市, 鹿児島
Helium has been used as the pressurant gas for the propellants. Because helium is a strategy substance and its soa
Helium has been used as the pressurant gas for the propellants. Because helium is a strategy substance and its soa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0e7466434e4e6e9a679dcbc23caa973a
http://id.nii.ac.jp/1696/00038801/
http://id.nii.ac.jp/1696/00038801/
Autor:
Asakawa, Hiroya
SPACE PROPULSION 2014 (May 19-22, 2014. Maritim Hotel), Cologne, Germany
資料番号: PA1510094000
資料番号: PA1510094000
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=jairo_______::0d74e258518dc6b08b2e1579232752a1
http://id.nii.ac.jp/1696/00039547/
http://id.nii.ac.jp/1696/00039547/