high altitude balloon, membrane structure, deployment, large space structure, structural vibration, solar sail, space propulsion system, attitude control, space exploration
その他のタイトル（英）
Static deployment of large membrane using a balloon
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
University of Tokyo School of Engineering
University of Tokyo School of Engineering
Tokai University Graduate School of Engineering
Tokyo Denki University Graduate School of Engineering
University of Tokyo School of Engineering
University of Tokyo School of Engineering
Aoyama Gakuin University Department of Mechanical Engineering, College of Science and Engineering
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
出版者
宇宙航空研究開発機構
出版者（英）
Japan Aerospace Exploration Agency (JAXA)
雑誌名
宇宙航空研究開発機構研究開発報告: 大気球研究報告
雑誌名(英)
JAXA Research and Development Report: Research Reports on High Altitude Balloons
ISAS/JAXA is studying a deployment method using centrifugal force for solar power sail mission. When a large membrane is deployed dynamically, it is twisted and vibrations are excited. Thus it is required to be deployed statically. The mechanisms for static deployment are developed. The static deployment of the square sail of diameter 20 m using a high altitude balloon is demonstrated. The pre-examination on ice rink is also performed. In this paper, the contents and results of these experiments are reported in detail.
大気球を用いた大型膜面の準静的展開実験
63732003.pdf
(1.33MB)
