发明名称 Satellitenantenne
摘要 A satellite aerial is hinged and rests, prior to reaching the orbit, in the space between the satellite interior and the heat shield (42). To position the aerial rod (43) automatically, after the heat shield has been removed, and to keep the aerial in the extended position, the rod (43) is hinged by a pin (41) to the inner conductor (44) of a coaxial lead which is guided in a dielectric block (50). When the heat shield (42) does not restrain the aerial, a compression spring (46) acts on a sleeve (45) made of insulating material inside the cap (47) and erects the aerial in the vertical position. The dotted lines show how the aerial is fixed in that position.
申请公布号 DE2003811(A1) 申请公布日期 1971.08.05
申请号 DE19702003811 申请日期 1970.01.28
申请人 SIEMENS AG 发明人 HOFMANN,PETER
分类号 B64G1/22;H01Q1/08 主分类号 B64G1/22
代理机构 代理人
主权项
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