@inproceedings{oai:jaxa.repo.nii.ac.jp:00013528,
 author = {山中, 富夫 and 居相, 政史 and 臼田, 武史 and 松永, 三郎 and Yamanaka, Tomio and Iai, Masafumi and Usuda, Takeshi and Matsunaga, Saburo},
 book = {宇宙利用シンポジウム　第23回　平成18年度, Space Utilization Research: Proceedings of the Twenty-third Space Utilization Symposium},
 month = {Mar},
 note = {An electro dynamic tether is the effective way to deorbit nano-satellite. The authors focused on tether deployment which is one of the fundamental technologies in this way and developed two small tether deployment mechanisms with different methods. One was marman band method and the other was a string hold method. Micro gravity tests were conducted with both methods to evaluate the mechanisms. Furthermore, the mechanism with a string hold method was installed in Cute-1.7 + APD (Avalanche Photo Diode), nano-satellite developed by authors and launched successfully., 資料番号: AA0063349030},
 pages = {113--116},
 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 = {超小型衛星用テザー伸展機構の設計と開発},
 year = {2007}
}