@inproceedings{oai:jaxa.repo.nii.ac.jp:00007588,
 author = {川勝, 康弘 and 森, 治 and 津田, 雄一 and 中谷, 幸司 and 多羅尾, 康太 and 川口, 淳一郎 and Kawakatsu, Yasuhiro and Mori, Osamu and Tsuda, Yuichi and Nakaya, Koji and Tarao, Kota and Kawaguchi, Junichiro},
 book = {第15回アストロダイナミクスシンポジウム講演後刷り集　2005, Proceedings of 15th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {本発表では、「インタセプタ」という呼称で現在構想中の10kg級の超小型探査機を用いた、小惑星フライバイミッションのミッション解析結果を報告する。今回は(1)静止衛星打上時に小型固体モータを装着したインタセプタを相乗りさせるミッション、(2)小型打上機体により複数のインタセプタを同時に打ち上げるミッション、の2つのミッション形態を想定し、軌道計画、運用シナリオなどを検討した結果を報告する。, Reported in this paper is the result of the mission analysis of asteroid flyby missions using miniature asteroid interceptors. Two types of mission concept are considered. The first is a mission concept with an interceptor boosted from GTO (Geostationary Transfer Orbit) by small solid rocket motor (assuming the piggy back launch of geostationary satellite). The second is a mission concept with four interceptors loaded on a mother carrier spacecraft, launched together and released on orbit to target four different asteroids. The results of the trajectory analysis and operation sequence investigation are reported in the paper., 資料番号: AA0063480023},
 pages = {141--146},
 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 = {Mission analysis of asteroid flyby exploration by miniature asteroid interceptors},
 year = {2006}
}