@inproceedings{oai:jaxa.repo.nii.ac.jp:00016481,
 author = {船見, 祐揮 and 嶋田, 徹 and Funami, Yuki and Shimada, Toru},
 book = {平成22年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2010},
 month = {},
 note = {平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Estimation of chamber pressure is necessary for the design of a hybrid rocket. Comprehension of combustion instability and regression rate behaviour is required in order to estimate chamber pressure. Characteristics of combustion instability and regression rate behaviour are called "internal ballistics". In this study, literature research of AIAA paper about hybrid rocket's internal ballistics is done to recognize technical problems of the evaluation of internal ballistics characteristic., 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: AA0065073034},
 publisher = {宇宙航空研究開発機構宇宙科学研究所, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {ハイブリッドロケット内部弾道特性評価技術の発展経緯と課題},
 year = {2011}
}