@inproceedings{oai:jaxa.repo.nii.ac.jp:00016616,
 author = {植田, 修一 and 平岩, 徹夫 and 竹腰, 正雄 and 谷, 香一郎 and 苅田, 丈士 and 永田, 晴紀 and Ueda, Shuichi and Hiraiwa, Tetsuo and Takegoshi, Masao and Tani, Koichiro and Kanda, Takeshi and Nagata, Harunori},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {Jan},
 note = {平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部), Space Transportation Symposium (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)),  Sagamihara, Kanagawa Japan, This paper presents an overview of the subsonic flight experiments for ejector-rocket using CAMUI-type hybrid-rocket. The flight experiment was planned to obtain ejector characteristics under subsonic flight condition, for developing design technology of rocket based combined-cycle engine. An ejector-duct was attached to the engine of the rocket. Two experimental vehicles were launched at 16th March 2009, from the coast of Taiki-town in Hokkaido island of Japan. Flight experiments were successfully conducted and ejector characteristics data at the flight condition were acquired., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0064741046},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {ハイブリッドロケットＣＡＭＵＩを利用したエジェクタロケットの亜音速飛行実験},
 volume = {平成21年度},
 year = {2010}
}