Saito Hirobumi, Mizuno Takahide, Tanaka Koji, SONE Yoshitsugu, FUKUDA Seisuke, SAKAI Shin-ichiro, OKUIZUMI Nobukats, MITA Makoto, FUKUSHIMA Yosuke, HIRAHARA Masafumi, ASAMURA Kazushi, SAKANOI Takeshi, MIURA Akira, IKENAGA Toshinori, MASUMOTO Yasunari
電子情報通信学会技術研究報告. SANE, 宇宙・航行エレクトロニクス 2007年4月9日 一般社団法人電子情報通信学会
This paper describes the on-orbit results and lessons learned of the small scientific satellite "INDEX" (REIMEI) for aurora observation and demonstration of advanced satellite technologies. REIMEI is a small satellite with 72kg mass, and is provided with three-axis attitude controlled capabilities for aurora observation. REIMEI was launched into a nearly sun synchronous polar orbit on Aug. 23^<rd>, 2005 (UT) from Baikonur, Kazakhstan by Dnepr rocket. REIMEI satellite functions satisfactorily on the orbit. Three axis control is achieved with accuracy of 0.05 deg. Multi-spectrum images of aurora are taken with 8Hz rate and 2 km spatial resolution to investigate the aurora physics. REIMEI is a small scientific satellite for aurora observation and advanced satellite technologies, and was launched into a nearly sun synchronous polar orbit on Aug. 23^<rd>, 2005 (UTC) from Baikonur, Kazakhstan by Dnepr rocket. REIMEI satellite functions satisfactorily on the orbit. The three-axis attitude control is achieved with accuracy of 0.05deg. REIMEI is performing the simultaneous observation of aurora images as well as particle measurements. REIMEI indicates that even a small satellite launched as a piggy-back can successfully perform the unique scientific mission purposes.