发明名称 Space Deployable Antenna Reflector
摘要 1. Technical Result Increase in accuracy of reflector baffle, simplification of manufacture and attachment to space apparatus. 2. Essence At the ends of the deployable elements of the pull-apart frame 3 of the baffle 2 of the reflector there are fixed spreader bars 18, to which from the outer side of the pull-apart frame a frame 10 is connected of the deployable cupola with elastic baffle attached thereon, so that there is capability of emerging with the pull-apart frame of the baffle. 3. Field of Application Radio engineering, in particular reflectors for big antennas.
申请公布号 GEP20053604(B) 申请公布日期 2005.08.25
申请号 GE2001AP04328 申请日期 2001.06.12
申请人 发明人 MEDZMARIASHVILI, ELGUDJA
分类号 H01Q15/20;H01Q15/16 主分类号 H01Q15/20
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