发明名称 Ausrichtungsvorrichung und Bordausrichtungsanlage
摘要 The thrust vector motor for a satellite has a support plate (2) with connecting arms (41-43) which are spaced around the mounting. Each arm has a flexible section (4) with one end (47) connected to the end of the support via a first connection with a single degree of freedom (9) and a second degree of freedom (48) connected to the load by a second coupling (10) with one degree of freedom. Claims include a space system using the mounting
申请公布号 DE60107510(T8) 申请公布日期 2006.06.08
申请号 DE2001607510T 申请日期 2001.09.04
申请人 SNECMA MOTEURS 发明人 CHATENET, LUC
分类号 B64G1/24;B64G1/66;B64G1/22;B64G1/26;B64G1/64;F16C11/12;F16H21/46;F16M11/12 主分类号 B64G1/24
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