@inproceedings{oai:jaxa.repo.nii.ac.jp:00016213,
 author = {五十地, 輝 and 前田, 祐義 and 橋本, 祐治 and 植松, 努 and 永田, 晴紀 and Isochi, Hikaru and Maeda, Hiroyoshi and Hashimoto, Yuji and Uematsu, Tsutomu and Nagata, Harunori},
 book = {平成24年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2012},
 month = {Jan},
 note = {平成24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県, Space Transportation FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Uematsu Electric Co., Ltd. has been developing CAMUI-type hybrid rockets in collaboration with Hokkaido University. In July 2012 a flight test with a 5000 N thrust class CAMUI-type rocket was conducted. Main objectives of this flight test were technology acquisition concerning supersonic flight, tracking/telemetry and command subsystem, and airframe recovery from sea-water. This paper describes the development outline of the propulsion system and airframe structure of the test vehicle., 形態: カラー図版あり, 形態: PDF, Translation title: Development of the propulsion system and airframe structure of 5000 N thrust class CAMUI-type hybrid rocket, Physical characteristics: Original contains color illustrations, Physical characteristics: PDF, 資料番号: AA0061856077, レポート番号: STCP-2012-077},
 publisher = {宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS), Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {推力5000N級CAMUI型ハイブリッドロケットの推進系及び機体構造の開発},
 year = {2013}
}