发明名称 Antenna system for low-earth-orbit satellites
摘要 The present invention regards an antenna system (1;5) comprising a reflection system that comprises a reflector (11;52) having a rotational symmetry with respect to an axis of symmetry (12;54). Moreover, the antenna system (1;5) also comprises an electronically steerable planar radiating array (13;53) that is arranged in a focal region (14;55) of the reflection system, has a rotational symmetry with respect to the axis of symmetry (12;54) and is operable to radiate a primary radiofrequency beam oriented in a predefined direction of illumination with respect to the axis of symmetry (12;54) in such a way as to cause a specific region of the reflector (11;52) to be illuminated by said primary radiofrequency beam. Said specific region of the reflector (11;52) is designed, when illuminated by said primary radiofrequency beam, to generate by reflection a secondary radiofrequency beam oriented in at least one predefined direction of transmission with respect to the axis of symmetry (12;54).
申请公布号 EP2485328(A1) 申请公布日期 2012.08.08
申请号 EP20120153175 申请日期 2012.01.30
申请人 THALES ALENIA SPACE ITALIA S.P.A. CON UNICO SOCIO 发明人 MIZZONI, ROBERTO;PERRINI, FRANCO;NOSCHESE, PAOLO;ZOLESI, MARCELLO
分类号 H01Q3/26;H01Q15/14;H01Q19/17;H01Q19/19 主分类号 H01Q3/26
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