Japan Aerospace Exploration Agency Institute of Space and Astronautical Science
University of Tokyo Graduate School
University of Tokyo Graduate School
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15回アストロダイナミクスシンポジウム講演後刷り集 2005
雑誌名(英)
Proceedings of 15th 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 clover typed sail of 20 m diameter 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.
Static deployment experiment of large membrane for solar sail spacecraft
