@inproceedings{oai:jaxa.repo.nii.ac.jp:00038778,
 author = {森下, 拓往 and 三浦, 尚幸 and 藤平, 耕一 and 関川, 知里 and 髙井, 元 and 鷲谷, 正史 and 井上, 浩一 and 成田, 伸一郎 and 松村, 祐介 and Morishita, Hiroyuki and Miura, Yoshiyuki and Fujihira, Koichi and Sekigawa, Chisato and Takai, Moto and Washiya, Masahito and Inoue, Koichi and Narita, Shinichiro and Matsumura, Yusuke},
 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, 鹿児島県, This paper describes the design and development status about “JAXA Small GPS/Whl Demo Box”, which is developed for on-orbit demonstration of small GPS receiver and reaction wheel on the International Space Station (ISS). This equipment will set to Japanese Experiment Module on the ISS. The GPS receiver and reaction wheel have already finished developing but not flown in space yet, so this is the first opportunity to evaluate their functions in space environment. In this paper, the differences of on-orbit demonstration between using small satellites, loaded as hosted payload on large satellites or using ISS is also described., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AC1600036000, レポート番号: JSASS-2015-4488},
 publisher = {日本航空宇宙学会(JSASS), The Japan Society for Aeronautical and Space Sciences (JSASS)},
 title = {JEM曝露部を利用した小型衛星用機器の軌道上実証装置の開発小型衛星用機器の軌道上実証装置の開発},
 year = {2015}
}