Evaluation of the effect of the compression stiffness and the bending stiffness on the deployment of a membrane-like spacecraft with the multi-particle method

Yuya Miyamoto, Osamu Mori, Nobukatsu Okuizumi, Yasutaka Satoh, Junichiro Kawaguchi

研究成果: Conference article査読

抄録

In this study, we modify multi-particle method, a calculation method for predicting membrane behaviour, for evaluating collision between membranes and the change in membrane compression and bending stiffness due to devices mounted on membrane. This modification is verified its validity by the consistency with the results of the experiments conducted in the previous study. Then, we investigate the changes in the deployment behaviour when the temperature and thickness of solar cells change.

本文言語English
論文番号IAC-19_C2_2_7_x51668
ジャーナルProceedings of the International Astronautical Congress, IAC
2019-October
出版ステータスPublished - 2019
外部発表はい
イベント70th International Astronautical Congress, IAC 2019 - Washington, United States
継続期間: 2019 10 212019 10 25

ASJC Scopus subject areas

  • 航空宇宙工学
  • 天文学と天体物理学
  • 宇宙惑星科学

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