Static deployment of large membrane of spinning solar sail using a balloon

Osamu Mori, Maki Shida, Jun'ichiro Kawaguchi, Shuhei Nishimaki, Michihiro Matsumoto, Yusuke Shibasaki, Fuminori Hanaoka, Masataka Arakawa, Masayuki Sugita

研究成果: Conference contribution

2 被引用数 (Scopus)

抄録

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 20m 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.

本文言語English
ホスト出版物のタイトルAmerican Astronautical Society - Space Flight Mechanics 2007 - Advances in the Astronautical Sciences, Proceedings of the AAS/AIAA Space Flight Mechanics Meeting
ページ1029-1040
ページ数12
出版ステータスPublished - 2007
外部発表はい
イベント17th Annual Space Flight Mechanics Meeting - Sedona, AZ, United States
継続期間: 2007 1 282007 2 1

出版物シリーズ

名前Advances in the Astronautical Sciences
127 PART 1
ISSN(印刷版)0065-3438

Conference

Conference17th Annual Space Flight Mechanics Meeting
国/地域United States
CitySedona, AZ
Period07/1/2807/2/1

ASJC Scopus subject areas

  • 航空宇宙工学
  • 宇宙惑星科学

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