@inproceedings{oai:jaxa.repo.nii.ac.jp:00016493,
 author = {高田, 淳史 and 福地, 亜宝郎 and 松浦, 新 and 宮川, 清 and 岡本, 久夫 and Takada, Atsushi and Fukuchi, Aporo and Matsuura, Shin and Miyakawa, Kiyoshi and Okamoto, Hisao},
 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, Authors have developed low melting temperature thermoplastic propellant (LTP) for the Next Generation Solid Rocket by using thermoplastic elastomer. For more improvement performance, aluminum (Al) addition to LTP was studied. They produced LTP with Al addition experimentally, which productivity, mechanical properties, and combustion properties were obtained. Al less than 16% and binder more than 18% were necessary to mixing and fusion molding. Regarding mentioned properties, best composition (Binder/AP/Al=18/66/16) was selected in this study., 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: AA0065073046},
 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 = {次世代固体ロケット用低融点熱可塑性推進薬のアルミ添加による高性能化},
 year = {2011}
}