@techreport{oai:jaxa.repo.nii.ac.jp:00006224,
 author = {松本, 甲太郎 and 佐々, 修一 and 若林, 幸子 and 星野, 健 and 松本, 康司 and 片山, 保宏 and 二宮, 哲次郎 and 濱田, 吉郎 and 四宮, 康雄 and Matsumoto, Kotaro and Sasa, Shuichi and Wakabayashi, Sachiko and Hoshino, Takeshi and Matsumoto, Koji and Katayama, Yasuhiro and Ninomiya, Tetsujiro and Hamada, Yoshiro and Shinomiya, Yasuo},
 month = {Jan},
 note = {Lunar Exploration and Utilization become the major trend in the world space development, in these couple of years. As the follow-on project of SELENE, we had studied the first Japanese moon lander as SELENE-B from 2001. In SELENE-B, the exploration of the vicinity of a central peak of a crater, and the sure obstacle avoidance and safe landing were the major mission objectives. Corresponding to the new world trend for international Lunar exploration, we have expanded our mission purpose and research targets from lunar science to lunar exploration and utilization. For these extended mission purposes, severe technological requirements should still be solved for the implementation of these new missions. The lunar lander has to detect obstacles, such as crater or rocks, and land at the safe area. After the landing, the investigation will be done on the very rocky and rough terrain. The lander system will be requested to survive against the very low temperature (around 80 K) during the Lunar night. This paper reports the current studies on these technological subjects for the future lunar base., 資料番号: AA0049057015, レポート番号: JAXA-SP-05-011},
 title = {月探査利用の研究:月軟着陸実験機に向けて},
 year = {2006}
}