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64234000.pdf2.08 MB
titleJAXA極低音キャビテーションタンネルの設備機能確認試験結果
Other TitleVerification test results fo the cryogenic cavitation tunnel in JAXA
Author(jpn)新井山, 一樹; 吉田, 義樹; 長谷川, 敏; 渡邉, 光男; 橋本, 知之; 島垣, 満; 菊田, 研吾; 永浦, 克司; 田村, 努
Author(eng)Niiyama, Kazuki; Yoshida, Yoshiki; Hasegawa, Satoshi; Watanabe, Mitsuo; Hashimoto, Tomoyuki; Shimagaki, Mitsuru; Kikuta, Kengo; Nagaura, Katsuji; Tamura, Tsutomu
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; 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; 航空宇宙技術振興財団
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); Space Transportation Propulsion Research and Development Center, Space Transportation Mission Directorate, Japan Aerospace Exploration Agency (JAXA); Foundation for Promotion of Japanese Aerospace Technology; Foundation for Promotion of Japanese Aerospace Technology
Issue Date2009-02-13
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-08-008
Publication date2009-02-13
Languagejpn
eng
AbstractTo clarify the thermodynamic effects on cavitation in cryogenic propellants, new Cryogenic Cavitation Tunnel (CCT) was constructed in the Cryogenic Inducer Test Facility at the Kakuda Space Center of JAXA. Liquid nitrogen is used as the working fluid for experiments of the thermodynamic effects on cavitation. The performance of the tunnel was confirmed to be well-satisfied from the verification test by using a cavitating orifice. In this article, the results of the verification test and the future program are presented.
Description形態: カラー図版あり
KeywordsCavitation, Cryogenic Fluids, Thermodynamic Effect, Temperature Depression
Document TypeTechnical Report
JAXA Category研究開発資料
ISSN1349-1121
NCIDAA11983593
SHI-NOAA0064234000
Report NoJAXA-RM-08-008
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/21835


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