@techreport{oai:jaxa.repo.nii.ac.jp:00006266,
 author = {中村, 揚介 and 加藤, 松明 and 吉原, 圭介 and 橋本, 英一 and Nakamura, Yosuke and Kato, Matsuaki and Yoshihara, Keisuke and Hashimoto, Hidekazu},
 month = {Jan},
 note = {The Space Technology Demonstration Research Center in JAXA has researched on the potential ability of 50-100 kg class small satellites which is used to demonstrate newly-developed components and advanced space technologies in space. We have a plan to develop several types of such small 'space demonstration satellites' as a series. MicroLabSat, the first one of the series, is a 50 kg class of spin stabilized satellite launched in December 2002 as a piggyback satellite on H-2A rocket. It has successfully completed all the planned experiments and continues healthy operation. Following MicroLabSat, we are developing MicroLabSat 2 with the three axis stabilized attitude control system. On the other hand, JAXA has started technology transfer program for SOHLA, which is the SME union in Kansai area, to develop a concise space demonstration satellite applying the MicroLabSat bus technology. In this paper, we will express the status and result of these micro-satellites for space technology demonstration., 資料番号: AA0049054010, レポート番号: JAXA-SP-05-008},
 title = {宇宙実証システムの研究},
 year = {2006}
}