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
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構研究開発資料
雑誌名(英)
JAXA Research and Development Memorandum
巻
JAXA-RM-08-008
発行年
2009-02-13
抄録（英）
To 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.
JAXA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
64234000.pdf
(2.13MB)
