@inproceedings{oai:jaxa.repo.nii.ac.jp:00038806,
 author = {淺川, 弘也 and 南里, 秀明 and 増田, 井出夫 and 石本, 真二 and 井上, 琢磨 and 石原, 新史 and 石崎, 真一郎 and 米本, 浩一 and Asakawa, Hiroya and Nanri, Hideaki and Masuda, Ideo and Ishimoto, Shinji and Inoue, Takuma and Ishihara, Shinji and Ishizaki, Shinichiro and Yonemoto, Koichi},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-14日. かごしま県民交流センター), 鹿児島市, 鹿児島, This paper reports the result of conceptual study on LOX/LNG(methane) engine for WIRES#015 (WInged Reusable Sounding rocket). LNG has better characteristics for rocket fuel, i.e. longer storage, lower cost and non-toxic. In particular, when applying LNG engine for booster stage of reusable launch vehicle (RLV), the vehicle size can be smaller and fuel cost can be reduced. Therefore, we have been studying on LNG engine for RLV. As part of this study, we plan to apply LNG engine to WIRES#015 and perform flight experiment to identify the challenges of LNG engine for RLV., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600075000, レポート番号: JSASS-2015-4250},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {小型有翼ロケット実験機(WIRES#015)への搭載を想定したLOX/LNG(メタン)エンジンの概念検討},
 year = {2015}
}