JAXA Repository / AIREX 未来へ続く、宙(そら)への英知
64231000.pdf3.19 MB
titleJAXA極低音インデューサ試験結果の概要
Other TitleOverview of experimental results of cryogenic inducer in JAXA
Author(jpn)吉田, 義樹; 渡邉, 光男; 長谷川, 敏; 橋本, 知之; 島垣, 満; 木村, 俊哉; 永浦, 克司; 菊田, 研吾; 笹尾, 好史; 風見, 佑介
Author(eng)Yoshida, Yoshiki; Watanabe, Mitsuo; Hasegawa, Satoshi; Hashimoto, Tomoyuki; Shimagaki, Mitsuru; Kimura, Toshiya; Nagaura, Katsuji; Kikuta, Kengo; Sasao, Yoshifumi; Kazami, Yusuke
Author Affiliation(jpn)宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター; 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター; 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター; 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター; 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター; 宇宙航空研究開発機構宇宙輸送ミッション本部宇宙輸送系推進技術研究開発センター; 航空宇宙技術振興財団; 東北大学流体科学研究所; 東北大学流体科学研究所; 東北大学流体科学研究所
Author Affiliation(eng)Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Foundation for Promotion of Japanese Aerospace Technology; Institute of Fluid Science, Tohoku University; Institute of Fluid Science, Tohoku University; Institute of Fluid Science, Tohoku University
Issue Date2008-12-26
PublisherJapan Aerospace Exploration Agency (JAXA)
宇宙航空研究開発機構
Publication titleJAXA research and development memorandum
宇宙航空研究開発機構研究開発資料
VolumeJAXA-RM-08-005
Publication date2008-12-26
Languagejpn
eng
AbstractTurbopump inducer, which is actually a high-precision, high-speed, sophisticated rotating impeller, is one of the key components of a liquid propellant rocket engine. On the other hand, the thermodynamic effect on cavitation is a favorable phenomenon in cryogenic fluids. It suppresses the growth of cavity since thermal imbalance appears around the cavity due to heat transfer for evaporation. Therefore, cavitation performance in cryogenic fluids is improved. In this article, some highlights about the thermodynamic effects on cavitating inducer carried out during the years 2004-2006 through the Cryogenic Inducer Test Facility in JAXA are presented.
Description形態: カラー図版あり
著者人数: 14人
KeywordsCavitation, Inducer, Cryogenic Fluid, Thermodynamic Effect
Document TypeTechnical Report
JAXA Category研究開発資料
ISSN1349-1121
NCIDAA11983593
SHI-NOAA0064231000
Report NoJAXA-RM-08-005
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/21308


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