| 发明名称 |
STRUCTURE DE DEPLOIEMENT DE PANNEAUX SOLAIRES POUR SATELLITE |
| 摘要 |
<p>A satellite deployment structure comprises panels (2) that are connected to a main body of a satellite and are rotatably connected to one another; and elastic insertion member (6) for prevention of vibration disposed in a clearance between each of the panels and in that between the main body and a panel adjacent to the main body when the panels are housed with them folded and layered.</p> |
| 申请公布号 |
FR2837168(B1) |
申请公布日期 |
2006.12.29 |
| 申请号 |
FR20020013771 |
申请日期 |
2002.11.04 |
| 申请人 |
MITSUBISHI DENKI KABUSHIKI KAISHA |
发明人 |
OZAWA TAKUO;OZAKI TSUYOSHI |
| 分类号 |
B64G1/44;B64G1/22;B64G1/64;B64G1/66 |
主分类号 |
B64G1/44 |
| 代理机构 |
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代理人 |
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| 主权项 |
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| 地址 |
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