@inproceedings{oai:jaxa.repo.nii.ac.jp:00017457,
 author = {Zhang, Feng-Yuan and 中山, 英一 and 服部, 豪 and 吉田, 悟 and 東, 伸幸 and 藤原, 俊隆 and 宮坂, 武志 and 斎藤, 彰 and 田麥, あづさ and Zhang, Feng-Yuan and Nakayama, Eiichi and Hattori, Tsuyoshi and Yoshida, Satoru and Azuma, Nobuyuki and Fujiwara, Toshitaka and Miyasaka, Takeshi and Saito, Akira and Tamugi, Azusa},
 book = {宇宙輸送シンポジウム　平成13年度, Proceedings of Space Transportation Symposium FY2001},
 month = {Apr},
 note = {An experiment research on pulse detonation engine (PDE), which is developed in Nagoya University, is conducted with hydrogen/air. The fuel and oxidizer are injected into the tube with the opposite directions and are mixed by the collision of the two jets. Some key issues, including valve operation, injection, mixing, filling repetition, timing, ignition and propagation are investigated. The PDE performance is also estimated and the specific impulse of about 2,000 s is derived based on the pressure history at the head end. PDE operation at 32 Hz is successfully conducted., 資料番号: AA0033392029},
 pages = {115--118},
 publisher = {宇宙科学研究所, The Institute of Space and Astronautical Science (ISAS)},
 title = {DDT短縮化にPDEの開発に向けて},
 year = {2002}
}