@article{oai:jaxa.repo.nii.ac.jp:00021664,
 author = {丸, 祐介 and 石川, 毅彦 and 坂東, 信尚 and 澤井, 秀次郎 and 清水, 成人 and 坂井, 真一郎 and 吉光, 徹雄 and 小林, 弘明 and 菊池, 政雄 and 山本, 信 and 福山, 誠二郎 and 岡田, 純平 and 菅, 勇志 and 梯, 友哉 and 福家, 英之 and 伊藤, 琢博 and 水島, 隆成 and 江口, 光 and Maru, Yusuke and Ishikawa, Takehiko and Bando, Nobutaka and Sawai, Shujiro and Shimizu, Shigehito and Sakai, Shinichiro and Yoshimitsu, Tetsuo and Kobayashi, Hiroaki and Kikuchi, Masao and Yamamoto, Shin and Fukuyama, Seijiro and Okada, Junpei and Kan, Yuji and Kakehashi, Yuya and Fuke, Hideyuki and Ito, Takahiro and Mizushima, Takanari and Eguchi, Hikaru},
 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 = {In this paper is presented a microgravity experiment system utilizing a high altitude balloon. The feature is a double shell structure of a vehicle that is dropped off from the balloon and a microgravity experiment section that is attached to the inside of the vehicle with a liner slider. Control with cold gas jet thrusters of relative position of the experiment section to the vehicle and attitude of the vehicle maintains fine microgravity environment. The design strategy of the vehicle is explained, mainly referring to differences from the authors' previous design. The result of the flight experiment is also shown to evaluate the characteristics of the presented system., 形態: 図版あり, Physical characteristics: Original contains illustrations, 資料番号: DS1540389004},
 pages = {257(25)--264(32)},
 title = {気球を利用した微小重力実験のための，一軸制御型機体システムの開発と飛行実験結果},
 volume = {63},
 year = {2015}
}