@inproceedings{oai:jaxa.repo.nii.ac.jp:00047342,
 author = {杉浦, 正彦 and 田辺, 安忠 and 菅原, 瑛明 and 木村, 桂大 and 竹川, 国之 and 大山, 聖 and 佐藤, 允 and 金崎, 雅博 and 岸, 祐希 and SUGIURA, Masahiko and TANABE, Yasutada and SUGAWARA, Hideaki and KIMURA, Keita and TAKEKAWA, Kuniyuki and OYAMA, Akira and SATO, Makoto and KANAZAKI, Masahiro and KISHI, Yuki},
 book = {宇宙航空研究開発機構特別資料: 流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2020オンライン論文集, JAXA Special Publication: Proceedings of Fluid Dynamics Conference / Aerospace Numerical Simulation Symposium 2020 Online},
 month = {Feb},
 note = {流体力学講演会/航空宇宙数値シミュレーション技術シンポジウム2020オンライン (2020年9月28日-30日. 日本航空宇宙学会 : 宇宙航空研究開発機構(JAXA)オンライン会議), 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), 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., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030013021, レポート番号: JAXA-SP-20-008},
 pages = {157--164},
 publisher = {宇宙航空研究開発機構(JAXA), Japan Aerospace Exploration Agency (JAXA)},
 title = {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},
 volume = {JAXA-SP-20-008},
 year = {2021}
}