@techreport{oai:jaxa.repo.nii.ac.jp:00002147,
 author = {徳留, 真一郎 and 八木下, 剛 and 羽生, 宏人 and 鈴木, 直洋 and 大毛, 康弘 and 嶋田, 徹 and Tokudome, Shinichiro and Yagishita, Tsuyoshi and Habu, Hiroto and Suzuki, Naohiro and Daimo, Yasuhiro and Shimada, Toru},
 month = {Feb},
 note = {無毒で常温貯蔵可能な液体推進剤として亜酸化窒素(N2O)／エタノールの組合せに着目し、それによる扱い易い液体推進系の実証研究を進めている。当面の目標として大気吸い込み式極超音速推進系の飛行試験に用いる加速用ロケットエンジンへの適用を目指しているが、その低温環境順応性を活かす衛星・探査機搭載推進系への応用も視野に入れている。これまでに、推力700N級の要素試験供試体を用いた燃焼試験を2シリーズ行って、エンジン噴射器設計のための有用なデータと運用特性を取得してきた。併せて、水冷式燃焼器による燃焼器壁面熱流束分布の測定や厚肉のシリカ繊維強化プラスチックSFRP(Silica Fiber Reinforced Plastic)製燃焼器を用いた燃焼試験によって燃焼器への耐熱複合材料適用の可能性も探っている。, A Nitrous Oxide (N2O)/ethanol propulsion system is distinguished as the liquid propulsion with non-toxic, user-friendly, and storable bipropellant. The current target of the present study is to build a quick-response and maneuverable main engine of a sounding-rocket like flying test bed which will be applied to the hypersonic air-breathing propulsion researches in the near future. The application to the spacecraft propulsion is also considered due to its compatibility in low-temperature operation environment. Two series of static firing tests were performed with 700 N class gas generator models so far. Current test results showed that valuable design data were collected and operational procedure was verified. Potential of application of composite materials to the combustion chamber was also examined from the chamber wall heat flux data obtained and the result of firing test using a thick SFRP (Silica Fiber Reinforced Plastic) chamber., 資料番号: AA0063882000, レポート番号: JAXA-RR-07-027},
 title = {亜酸化窒素(N2O)/エタノール推進系の実験研究},
 year = {2008}
}