@article{oai:muroran-it.repo.nii.ac.jp:00008562,
 author = {湊,  亮二郎 and MINATO, Ryojiro and 東野,  和幸 and HIGASHINO, Kazuyuki and 棚次,  亘弘 and TANATSUGU, Nobuhiro},
 journal = {室蘭工業大学紀要, Memoirs of the Muroran Institute of Technology},
 month = {Mar},
 note = {application/pdf, Supersonic Unmanned Aerial Vehicle Project proceeds in Aerospace Plane Research Center at Muroran Institute Technology. The Gas Generator cycled Air Turbo Ramjet Engine is the most promising candidate for propulsion engine for this UAV. For this GG-ATR engine, its fuel and oxidizer are bio-ethanol and liquefied oxygen (LOX), respectively. The present paper describes about GG-ATR engine cycle analysis, design and manufacturing of engine components, ground test facilities. In addition, the authors describe about future study plan for ground test of GG-ATR engine., 特集 : 航空宇宙機システム研究センターにおける開発研究2 : 1. オオワシII飛行にむけて並びに関連技術の研究開発（推進系）},
 pages = {23--28},
 title = {オオワシ2号機推進システムに関する研究},
 volume = {64},
 year = {2015},
 yomi = {ミナト, リョウジロウ and ヒガシノ, カズユキ and タナツグ, ノブヒロ}
}