@inproceedings{oai:jaxa.repo.nii.ac.jp:00007758,
 author = {佐野, 成寿 and 大塚, 浩仁 and 森田, 泰弘 and 平木, 講儒 and Sano, Naruhisa and Otsuka, Hirohito and Morita, Yasuhiro and Hiraki, Koju},
 book = {平成15年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers},
 month = {Feb},
 note = {ロケットをパラグライダで回収する技術の実証のためのロケット回収実験機を説明する。また、2003年2月に実施した、ヘリコプタから吊り下げた状態での機体の制御系の機能や性能を確認した結果を示す。ヘリコプタによる高空からの投下試験は、2004年2月に実施予定である。, This rocket recovery demonstrator vehicle is scheduled to launch in February 2004. This demonstrator vehicle is planned to perform the guidance by the paraglider with small rocket vehicle. This vehicle will be dropped from a helicopter at 2,000 m altitude in February 2004. Some functions and performances of this demonstrator were tested at February 2003. The outline of this flight test in 2004 is shown and the results of the tests under the condition suspended from the helicopter in February 2003 are shown., 資料番号: AA0046652057},
 pages = {352--355},
 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/ISAS)},
 title = {Test results of rocket recovery demonstrator vehicle suspended from helicopter},
 year = {2004}
}