Experiment of deployment and attitude control for spinning solar power sail using balloon

Fuminori Hanaoka, Masataka Arakawa, Shunsuke Okada, Yusuke Shibasaki, Yoji Shirasawa, Osamu Mori, Maki Shida, Yuichi Tsuda, Jun'ichiro Kawaguchi

研究成果: Conference contribution

抄録

The proposed balloon experiment for deploying large-sized membrane, which is intended to be shown in this paper, is postponed to September, 2008. We are now designing a new structure and mechanism of a spacecraft which is to be validated at the balloon experiment. We proposed "Multi-step deployment" of membrane in this paper, which reduces the risk of complexity of the deploying system compared to conventional system. In addition, we analyzed the feasibility of attitude control required for orbital maneuver with conventional chemical thruster and positively solved. The amount of propellant is also calculated and found to be feasible. The system we discussed in this paper is to be equipped with a newly designed spacecraft planned in 2010s. Copyright IAF/IAA. All rights reserved.

本文言語English
ホスト出版物のタイトルInternational Astronautical Federation - 58th International Astronautical Congress 2007
ページ4142-4150
ページ数9
出版ステータスPublished - 2007
外部発表はい
イベント58th International Astronautical Congress 2007 - Hyderabad, India
継続期間: 2007 9 242007 9 28

出版物シリーズ

名前International Astronautical Federation - 58th International Astronautical Congress 2007
6

Other

Other58th International Astronautical Congress 2007
国/地域India
CityHyderabad
Period07/9/2407/9/28

ASJC Scopus subject areas

  • 宇宙惑星科学
  • 航空宇宙工学

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