发明名称 |
System for securing an articulated assembly of elements on a spacecraft |
摘要 |
A system for securing deployable elements, such as solar panels, on a structure, such as a spacecraft, with the aid of a through rod. A mechanism is provided for releasing the through rod from the elements at the moment of deployment thereof, then for returning the rod into its initial position with respect to the outer element.
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申请公布号 |
US4936367(A) |
申请公布日期 |
1990.06.26 |
申请号 |
US19890313064 |
申请日期 |
1989.02.22 |
申请人 |
AEROSPATIALE SOCIETE NATIONALE INDUSTRIELLE |
发明人 |
MARELLO, GEORGES;AUTERNAUD, JACQUES |
分类号 |
B64G1/44;B64G1/22;B64G1/64 |
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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