@techreport{oai:jaxa.repo.nii.ac.jp:00002740,
 author = {遠山, 伸一 and 芳仲, 敏成 and Toyama, Shinichi and Yoshinaka, Toshinari},
 month = {Oct},
 note = {Before the ignition and restart of the 2nd stage engines of H-2A rocket, the turbo-pumps must be sufficiently cooled by liquid Oxygen and Hydrogen preliminary. But, the cooling duration was determined by the experimental and previous flight data. Thermal analyses have been conducted to predict the duration precisely and estimate the necessary quantities of liquid Oxygen and Hydrogen., 資料番号: AA0047944009, レポート番号: JAXA-RM-04-009},
 title = {H-2A第2段ターボポンプの予冷熱解析},
 year = {2004}
}