@inproceedings{oai:jaxa.repo.nii.ac.jp:00016462,
 author = {中田, 大将 and 神津, 亜実 and 矢島, 淳 and 西根, 賢治 and 東野, 和幸 and 棚次, 亘弘 and Nakata, Daisuke and Kozu, Ami and Yjima, Jun and Nishine, Kenji and Higashino, Kazuyuki and Tanatsugu, Nobuhiro},
 book = {平成22年度宇宙輸送シンポジウム: 講演集録, Proceedings of Space Transportation Symposium: FY2010},
 month = {},
 note = {平成22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 相模原市, 神奈川県, Space Transportation FY2010 (January 20-21, 2011. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS)), Sagamihara, Kanagawa Japan, Rocket sled is well known device that enables us to measure aerodynamic effect in full-scale model. In United States, rocket sleds have been utilized for the validation experiments of many practical aircrafts and spacecrafts. Muroran Institute of Technology constructed 1.4 m in width, 300 m in length test track and started the operation of full-scale rocket sled. As an acceleration system, tandem hybrid rockets are used. An optimum deceleration system within the limited track length was attempted by stepwise water braking system. Frequent reconsideration of operation procedure reduced the turn around time to 2 hour with 4 people., 形態: カラー図版あり, 形態: CD-ROM1枚, Physical characteristics: Original contains color illustrations, Note: One CD-ROM, 資料番号: AA0065073015},
 publisher = {宇宙航空研究開発機構宇宙科学研究所, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)},
 title = {ハイブリッドロケット搭載高速走行軌道実験装置},
 year = {2011}
}