@inproceedings{oai:jaxa.repo.nii.ac.jp:00014425,
 author = {藤田, 和央 and 鈴木, 俊之 and 高柳, 大樹 and 加納, 希生 and 橘, 省吾 and 川口, 淳一郎 and Fujita, Kazuhisa and Suzuki, Toshiyuki and Takayanagi, Hiroki and Kano, Kiyo and Tachibana, Shogo and Kawaguchi, Junichiro},
 book = {宇宙航行の力学シンポジウム, Symposium on Flight Mechanics and Astrodynamics},
 month = {Dec},
 note = {宇宙航行の力学シンポジウム(平成20年度)(2008年12月4～5日、宇宙航空研究開発機構宇宙科学研究本部), Symposium on Flight Mechanics and Astrodynamics 2008 (December 4-5, 2008. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)), Sagamihara, Kanagawa Japan, Feasibility assessment of a Martian aero-flyby sample return system for JAXA's future Martian exploration has been conducted. In the mission scenario, the vehicle enters the Martian atmosphere, collects the Martian dust and atmosphere during the atmospheric flight, exits the Martian atmosphere, and is inserted into a parking orbit from which the return system is departed for the earth. In order to accomplish controlled flight and successful orbit insertion, aerocapture technologies are introduced into the vehicle guidance and control system. A conceptual design is presented as a result of the preliminary design study., 資料番号: AA0064729002},
 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)},
 title = {エアロキャプチャによる火星ダストサンプルリターン機の検討},
 volume = {平成20年度},
 year = {2009}
}