@inproceedings{oai:jaxa.repo.nii.ac.jp:00007667,
 author = {山川, 宏 and 川勝, 康弘 and 安部, 正真 and 矢野, 創 and 森本, 睦子 and Yamakawa, Hiroshi and Kawakatsu, Yasuhiro and Abe, Masanao and Yano, Hajime and Morimoto, Mutsuko},
 book = {平成16年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers},
 month = {Mar},
 note = {ポスト「はやぶさ」としての小天体探査計画の提案の1つとして、複数小惑星からのサンプルリターンミッションの軌道計画を行った。, Sample return missions to multiple near-Earth asteroids are investigated assuming solar electric propulsion as a propulsive means. The objective of the trajectory design is not only to maximize the number of the target asteroids and the payload mass of the spacecraft, but also to make the flight time up to the Earth return as short as possible for quick science return., 資料番号: AA0047897034},
 pages = {193--199},
 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 = {Multiple near-Earth asteroid sample return mission in the next decade: Preliminary design},
 year = {2005}
}