Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Japan Aerospace Exploration Agency (JAXA)
Ryoyu Systems Co., Ltd.
Japan Aerospace Exploration Agency (JAXA)
Kogakuin University
Tokyo Metropolitan University
Tokyo Metropolitan University
Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online (September 28-30, 2020. The Japan Society for Aeronautical and Space Sciences : Japan Aerospace Exploration Agency (JAXA), Online meeting)
抄録（英）
A conceptual study of Mars helicopter for the purpose of observation of the oval tunnels on the Mars has been carried out. Mainly from the limit of the storage size together with the Mars rover, a hexa-rotor drone is proposed with a gross weight of 3 kg. Each rotor consists of 4 blades while the rotor diameter is 460 mm. Optimized design of the airfoil to achieve higher hovering performance is being performed.
内容記述
形態: カラー図版あり
内容記述（英）
Physical characteristics: Original contains color illustrations
火星ヘリコプタ用ロータブレード平面形状の空力的最適設計
AA2030013021.pdf
(3.67MB)
