@inproceedings{oai:jaxa.repo.nii.ac.jp:00014426,
 author = {高柳, 大樹 and 藤田, 和央 and Takayanagi, Hiroki and Fujita, Kazuhisa},
 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, An aerodynamic control system using movable flaps extending from the primary aeroshell is proposed to broaden a window of successful orbit insertion. Aerodynamic coefficients of the vehicle with and without flaps are measured in JAXA hypersonic wind tunnel. From these values, database of the aerodynamic coefficients with the angle of flaps variations were estimated by fitting equations on the basis of the modified Newton method., 資料番号: AA0064729003},
 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 = {フラップ付エアロキャプチャシェルの空力係数の推定},
 volume = {平成20年度},
 year = {2009}
}