@inproceedings{oai:jaxa.repo.nii.ac.jp:00003763,
 author = {戎崎, 俊一 and Quinn, Mark N. and 和田, 智之 and Piotrowski, Lech Wiktor and 滝澤, 慶之 and Casolino, Marco and Bertaina, Mario and Gorodetzky, Philippe and Parizot, Etienne and 田島, 俊樹 and Ebisuzaki, Toshikazu and Quinn, Mark N. and Wada, Satoshi and Piotrowski, Lech Wiktor and Takizawa, Yoshiyuki and Casolino, Marco and Bertaina, Mario and Gorodetzky, Philippe and Parizot, Etienne and Tajima, Toshiki},
 book = {宇宙航空研究開発機構特別資料: 第6回スペースデブリワークショップ講演資料集, JAXA Special Publication: Proceedings of the 6th Space Debris Workshop},
 month = {Mar},
 note = {第6回スペースデブリワークショップ (2014年12月17日-19日. 宇宙航空研究開発機構調布航空宇宙センター(JAXA)(CAC)), 調布市, 東京, 6th Space Debris Workshop (December 17-19, 2014. Chofu Aerospace Center, Japan Aerospace Exploration Agency (JAXA)(CAC)), Chofu, Tokyo, Japan, We present here a plan in 3 steps to design an orbiting debris remediation system comprised of a super-wide field-of-view telescope and a novel laser system operating from the International Space Station (ISS). The EUSO (Extreme Universe Space Observatory) telescope has been designed for operation onboard the ISS for the detection of ultra-high energy cosmic rays. Equipped with 2.5 m optics and a field of view of plus or minus 30 degrees, the EUSO module can also be utilized for the detection of high velocity fragmentation debris in orbit near the ISS. Once detected, the CAN laser system will deliver a sequence of pulses to the debris surface inducing ablation and hence momentum impulse to reduce its velocity. The range of the detection/removal operation can be as large as 100 km. We will use a step by step approach employing ISS : 1) Proof of principle demonstration of the detection (and, if possible, laser impulse technology) with ISS based small prototype 2) Technical demonstrator debris removal that consists of the EUSO telescope for the detection and a 1.5 m Cassegrain telescope with a space CAN laser for tracking and impulse delivery for debris re-entry, and 3) A free-flyer mission dedicated to debris remediation in a polar orbit with the altitude approximately 800 km., 著者人数: 12名, 形態: カラー図版あり, Number of authors: 12, Physical characteristics: Original contains color illustrations, 資料番号: AA1530025033, レポート番号: JAXA-SP-14-013},
 pages = {427--445},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {Remediation of cm-size space debris from the International Space Station},
 volume = {JAXA-SP-14-013},
 year = {2015}
}