@article{oai:jaxa.repo.nii.ac.jp:00021737,
 author = {高橋, 智也 and 杉浦, 裕樹 and 渡辺, 礼奈 and 安藤, 龍 and 宮嵜, 武 and 手塚, 亜聖 and Takahashi, Tomoya and Sugiura, Hiroki and Watanabe, Reina and Ando, Ryu and Miyazaki, Takeshi and Tezuka, Asei},
 issue = {6},
 journal = {日本航空宇宙学会論文集, Journal of the Japan Society for Aeronautical and Space Sciences},
 month = {Dec},
 note = {Almost all re-entry capsules such as HAYABUSA re-entry capsule are dynamically unstable in transonic region. We researched dynamic stability characteristics of Mars entry capsule (70 deg sphere-cone capsule model) at low speed. In order to avoid significant sting interference, the tests were conducted using magnetic suspension balance system (MSBS). Angle of attack and Reynolds number effects on drag coefficients were measured. Dynamic stability derivatives were measured by forced oscillation method. Drag coefficients were barely affected by Reynolds number and angle of attack. The dynamic stability derivatives of Mars entry capsule were small negative value. These results showed that Mars entry capsule was slightly dynamically unstable., 形態: 図版あり, Physical characteristics: Original contains illustrations, 資料番号: DS1640260001},
 pages = {289(1)--295(7)},
 title = {磁力支持を用いた火星探査カプセルの動安定計測},
 volume = {64},
 year = {2016}
}