Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
University of Tokyo Graduate School
University of Tokyo Graduate School
Tokai University Graduate School
Tokyo Denki University Graduate School
University of Tokyo Graduate School
University of Tokyo Graduate School
University of Tokyo Graduate School
University of Tokyo Graduate School
Aoyama Gakuin University
出版者
宇宙航空研究開発機構宇宙科学研究本部
出版者（英）
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)
雑誌名
第16回アストロダイナミクスシンポジウム講演後刷り集 2006
雑誌名(英)
Proceedings of 16th Workshop on JAXA Astrodynamics and Flight Mechanics
ISAS/JAXA is studying a deployment method using centrifugal force for solar sail mission. The larger sail is required to be deployed statically as for actual spacecraft. We scheduled to deploy the square sail of diameter 20 m using a high altitude balloon. In this paper, the mechanisms for static first and second stage deployments are proposed and developed experiment system is introduced. And the operation and results are shown in detail.
Asymmetric deployment dynamics of large membrane
