@article{oai:muroran-it.repo.nii.ac.jp:00008560,
 author = {HIGUCHI,  Ken and 樋口,  健 and 勝又,  暢久 and KATSUMATA, Nobuhisa},
 journal = {室蘭工業大学紀要, Memoirs of the Muroran Institute of Technology},
 month = {Mar},
 note = {application/pdf, Technological research and development on the structure system of the supersonic aircraft are required to construct the supersonic flying test bed (FTB). Lightweight and high performance composite materials will be used where possible portions of the structures. The structure must be designed considering various interfaces, such as aerodynamic performance for take-off/landing and supersonic flight, guidance and control for autonomous flight, wireless communications for flight information, propulsion system components, thermal protection for onboard equipment over a broad range of temperatures from cryogenic to very high temperature, impact loading due to landing shock, and flight maneuvability, along with recovery/reusability. The circumstances, the present state of the structure design, and the required developmental research are summarized here, and the remaining problems for the design of flight model of Oowashi No.2 are presented., 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 : 3. オオワシII飛行にむけて並びに関連技術の研究開発（機体、構造系）},
 pages = {39--44},
 title = {オオワシⅡ構造系開発},
 volume = {64},
 year = {2015},
 yomi = {ヒグチ, ケン and カツマタ, ノブヒサ}
}