发明名称 |
ARTIFICIAL SATELLITE |
摘要 |
A plurality of panels (2 to 10) are coupled rotatably by a hinge mechanism (21a). The panels are folded when a rocket loaded with the panels is launched and unfolded in space after the artificial satellite is released. Each of the panels (2 to 10) is loaded with at least functional elements such as a solar panel, a battery, an attitude control device and a communication device separately or together. The devices loaded on the panels are electrically connected to each other. <IMAGE>
|
申请公布号 |
EP1559649(A1) |
申请公布日期 |
2005.08.03 |
申请号 |
EP20030758838 |
申请日期 |
2003.10.23 |
申请人 |
NAKASUKA, SHINICHI;SAKURA TECHNOLOGY DEVELOPMENT CO., LTD. |
发明人 |
NAKASUKA, SHINICHI |
分类号 |
B64G1/10;B64G1/22;B64G1/24;B64G1/42;B64G1/44;B64G1/66;(IPC1-7):B64G1/44 |
主分类号 |
B64G1/10 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|