发明名称 DUAL ANTENNA WHICH CAN SEPARATING FOR ROCKET
摘要 PURPOSE: A separable dual antenna for a rocket is provided to improve a success rate of a rocket launch by maintaining the optimum electric wave sensitivity after separation by respectively including separable antennas inside and outside a nose faring. CONSTITUTION: A mount unit(10) forms the inside of a rocket. A nose faring(20) is separable from the rocket and surrounds the mount unit. A transceiver system(30) is formed on the mount unit. An internal antenna(40) is installed in the inner side of the nose faring and is connected to the transceiver system to amplify the transmission and reception sensitivity of the transceiver system. An external antenna(50) is installed on the outer side of the nose faring and is connected to the internal antenna to amplify the transmission and reception sensitivity of the transceiver system.
申请公布号 KR101024405(B1) 申请公布日期 2011.03.23
申请号 KR20090132617 申请日期 2009.12.29
申请人 KOREA AEROSPACE RESEARCH INSTITUTE 发明人 LEE, KYUNG WON;YI, MOO KEUN
分类号 H01Q1/28;H01Q1/22;H01Q1/27 主分类号 H01Q1/28
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