@inproceedings{oai:jaxa.repo.nii.ac.jp:00011293,
 author = {水野, 貴秀 and 福田, 盛介 and 坂井, 智彦 and 高原, 卓也 and 浜田, 裕介 and 井高, 裕次郎 and Mizuno, Takahide and Fukuda, Seisuke and Sakai, Tomohiko and Takahara, Takuya and Hamada, Yusuke and Idaka, Yujiro},
 book = {第5回宇宙科学シンポジウム, Proceedings of the 5th Space Science Symposium},
 month = {Sep},
 note = {Institute of Space and Astronautical Science JAXA develops the radio altimeter and velocity meter (landing radar) that is one of mandatory navigation sensor for a planetary lander. The landing radar can measure its relative altitude and speed from planetary surface by C band (4.3 GHz) pulse. The maximum range of this landing radar is 3.5 km. In this paper, we describe functions and parameters of the BBM Radar and the dynamic flight experiment using aircraft., 資料番号: AA0049122039},
 pages = {165--168},
 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 = {月惑星探査機搭載用着陸レーダの開発},
 year = {2005}
}