@inproceedings{oai:jaxa.repo.nii.ac.jp:00013402,
 author = {藤井, 裕矩 and 渡部, 武夫 and 草谷, 大郎 and 小島, 広久 and 小山, 孝一郎 and 佐々木, 進 and 田中, 孝治 and 阿部, 琢美 and 下山, 学 and 山極, 芳樹 and Fujii, Hironori A. and Watanabe, Takeo and Kusagaya, Tairo and Kojima, Hirohisa and Oyama, Koichiro and Sasaki, Susumu and Tanaka, Koji and Abe, Takumi and Shimoyama, Manabu and Yamagiwa, Yoshiki},
 book = {宇宙利用シンポジウム　第24回　平成19年度, Space Utilization Research: Proceedings of the Twenty-fourth Space Utilization Symposium},
 month = {Mar},
 note = {Two projects are introduced in this paper to verify the performance of space tether technology. A sounding rocket will be launched in the summer of 2009 to deploy a bare electro-dynamic tape tether having a length of 300 m. The other project to verify the space tether technology is a small satellite to deploy a bare 25 km electro-dynamic tape tether, and the launch is expected in 2013 with employing a new solid motor rocket. These verifications of tether technology will lead to a large numbers of applications of space tether technology and some future projects are also introduced., 資料番号: AA0063706026},
 pages = {113--114},
 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 = {ベア導電テープテザーの理工学に関する観測ロケット実験},
 year = {2008}
}