抜粋
Possible construction scenarios of future large space systems such as solar power satellites based on the combination of robotic and deployment construction schemes are introduced. As their deployable elements light weight membrane array structures actuated by extendible booms are considered, and several folding patterns of large solar cell membrane surfaces are presented. Some deployment aspects on a laboratory scale conceptual one-dimensional array model are also shown.
| 元の言語 | English |
|---|---|
| ホスト出版物のタイトル | 61st International Astronautical Congress 2010, IAC 2010 |
| ページ | 7443-7450 |
| ページ数 | 8 |
| 巻 | 9 |
| 出版物ステータス | Published - 2010 |
| イベント | 61st International Astronautical Congress 2010, IAC 2010 - Prague 継続期間: 2010 9 27 → 2010 10 1 |
Other
| Other | 61st International Astronautical Congress 2010, IAC 2010 |
|---|---|
| 市 | Prague |
| 期間 | 10/9/27 → 10/10/1 |
フィンガープリント
ASJC Scopus subject areas
- Aerospace Engineering
- Astronomy and Astrophysics
これを引用
Fujii, R., Katsumata, N., Natori, M. C., & Yamakawa, H. (2010). Structure concepts and characteristics of advancd lightweight solar cell array systems. ： 61st International Astronautical Congress 2010, IAC 2010 (巻 9, pp. 7443-7450)