@inproceedings{oai:jaxa.repo.nii.ac.jp:00013770,
 author = {谷, 佳子 and 吹田, 義一 and 田中, 健司 and 佃, 芳行 and 寺嶋, 昇 and 山内, 庄司 and 今川, 吉郎 and Tani, Yoshiko and Suita, Yoshikazu and Tanaka, Kenji and Tsukuda, Yoshiyuki and Terajima, Noboru and Yamauchi, Shoji and Imagawa, Kichiro},
 book = {宇宙利用シンポジウム　第21回　平成16年度, Space Utilization Research: Proceedings of the Twenty-first Space Utilization Symposium},
 month = {Mar},
 note = {Since the operation period of a space station is very as long as ten years or more, the space station may receive damage by the collision such as space debris, space robot and space transportation system. Therefore, establishment of the repair technology of a space station is expected. The simulated space station wall damaged by collision was made as an experiment, and the total leak air through damaged wall was estimated. In order to research the repair method in a pressurized module, repair experiment of simulated workpiece damaged by collision was performed by the various tapes, carbon sheet and welding. The evaluation method about some kinds of repair was investigated by the Analytic Hierarchy Process., 資料番号: AA0048095041},
 pages = {178--181},
 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 = {衝突損傷を受けた宇宙ステーション壁の修理技術},
 year = {2005}
}