@techreport{oai:jaxa.repo.nii.ac.jp:00002598,
 author = {新井山, 一樹 and 吉田, 義樹 and 長谷川, 敏 and 渡邉, 光男 and 橋本, 知之 and 島垣, 満 and 菊田, 研吾 and 永浦, 克司 and 田村, 努 and Niiyama, Kazuki and Yoshida, Yoshiki and Hasegawa, Satoshi and Watanabe, Mitsuo and Hashimoto, Tomoyuki and Shimagaki, Mitsuru and Kikuta, Kengo and Nagaura, Katsuji and Tamura, Tsutomu},
 month = {Feb},
 note = {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., 形態: カラー図版あり, 資料番号: AA0064234000, レポート番号: JAXA-RM-08-008},
 title = {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},
 year = {2009}
}