@inproceedings{oai:jaxa.repo.nii.ac.jp:00038827,
 author = {野崎, 健太 and 壹岐, 賢太郎 and 河本, 聡美 and 森野, 美樹 and Nozaki, Kenta and Iki, Kentaro and Kawamoto, Satomi and Morino, Yoshiki},
 book = {第59回宇宙科学技術連合講演会講演集, Proceedings of 59th Space Sciences and Technology Conference},
 month = {Oct},
 note = {第59回宇宙科学技術連合講演会（2015年10月7日-9日. かごしま県民交流センター), 鹿児島市, 鹿児島, The increase of space debris is becoming serious and active removal of large space debris from crowded economically useful orbits is required. The Japan Aerospace Exploration Agency (JAXA) has been investigating the electrodynamic tether (EDT) system. Deploying a several kilo-meter tether is necessary in order to obtain sufficient thrust for large debris removal. Compared to deploying several hundred meters, deployment velocity increases and tether may be severed by the tension over tensile strength. The purpose of this study is to evaluate the simple spool-type reels and brake mechanisms for reducing deployment velocity with bare tether. First, by ground experiments, we modeled deployment friction of the spool-type reel deployed from the outside and of brake mechanisms for limiting exit diameter of reel case. Then, the models were applied to numeric simulations assuming a several kilo-meter deployment on orbit and we estimated the required value of the deployment friction and braking model., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600096000, レポート番号: JSASS-2015-4677},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {デブリ除去のための導電性テザー伸展におけるブレーキ機構の検討},
 year = {2015}
}