@inproceedings{oai:jaxa.repo.nii.ac.jp:00016742,
 author = {多屋, 公平 and 平井, 伴実 and 油井, 章宏 and 牧野, 隆 and 森, 初男 and 呉, 宏堯 and 野口, 裕一 and Taya, Kohei and Hirai, Tomomi and Yui, Akihiro and Makino, Takashi and Mori, Hatsuo and Kure, Hirotaka and Noguchi, Yuichi},
 book = {宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium},
 month = {},
 note = {平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部), Applying the highly-reliability design approach, the authors conducted conceptual designing of a space tourism vehicle in an appropriate method to fulfill customer requests. Consequently, the high-performance, robust and cost-optimized vehicle concept has been achieved., 形態: カラー図版あり, 資料番号: AA0064292049},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)},
 title = {統合設計手法による観光用弾道宇宙船の概念設計},
 volume = {平成20年度},
 year = {2009}
}