Dynamic and static deployment motions of spin type solar sail

Osamu Mori, Yuichi Tsuda, Maki Shida, Jun'ichiro Kawaguchi

研究成果: Conference article査読

9 被引用数 (Scopus)

抄録

ISAS/JAXA is studying a deployment method using centrifugal force for solar sail mission. In this paper, the clover type sail is investigated. The deployment sequence consists of two stages. In order to analyze the motion of the dynamic deployment, S-310 flight experiment is conducted. In this experiment, the clover type sail of 10 m diameter is deployed dynamically. Numerical simulations by multi-particle model are also conducted to analyze the complicated motion. The experiment and simulation results are compared with each other to validate the analytical model. On the other hand, we schedule to conduct a balloon experiment. The clover type sail of 20 m diameter is deployed statically. The mechanisms for first stage and second stage deployments are introduced.

本文言語English
ページ(範囲)117-122
ページ数6
ジャーナルEuropean Space Agency, (Special Publication) ESA SP
548
出版ステータスPublished - 2004
外部発表はい
イベント18th International Symposium on Space Flight Dynamics - Munich, Germany
継続期間: 2004 10 112004 10 15

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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