Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
University of Tokyo School of Engineering
University of Tokyo School of Engineering
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
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
One of the most important assignments of the solar powered sail proposed in ISAS/JAXA is the static deployment of its membrane whose diameter is about 50 m. The demonstration of the deployment mechanism is performed using a balloon. First, the sail shape and its folding pattern are investigated by the dynamic deployment using a spinning table. Next, the deployment motion is analyzed by numerical simulations using multi-particle model in order to decide the sail size. Finally, the experiment system is introduced and the experiment results are shown in detail.
大気球を用いたソーラーセイル膜面の準静的展開実験
49046003.pdf
(7.69MB)
