Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Institute of Fluid Science, Tohoku University
Kanazawa University
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Kyushu University
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Kyushu Institute of Technology
Kanazawa Institute of Technology
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)
Airplane for Mars exploration is a new Mars observation platform that enables wide-range observation from low altitude. To establish high-altitude flight test system using JAXA's high-altitude balloon and to obtain aerodynamic data of an airplane for Mars exploration, high altitude flight test of the airplane was conducted. This paper explains summary of the flight test and compares the obtained aerodynamic data (lift and drag coefficient and lift-to-drag ratio) with wind tunnel data.
内容記述
著者人数: 16名
形態: カラー図版あり
内容記述（英）
Number of authors: 16 (JAXA staff: Motoda, Toshikazu ; Takeuchi, Shinsuke ; Kamata, Yukio ; Otsuki, Masatsugu ; Fujii, Kozo)
Physical characteristics: Original contains color illustrations
高高度飛行試験による火星飛行機の空力データの取得
AA1630045004.pdf
(9.03MB)
