发明名称 ROLLING DUAL MODE MISSILE
摘要 The system comprises a cylindrical missile body mounted at the front a hemispherical dome capable of passing infrared radiation. Two radio frequency antennas such as telescoping dielectric polystyrene rods are mounted diametrically opposed at the front of the missile body. A spinning magnetic gyroscope arrangement having optical elements to receive in frared radiation is mounted behind the dome. The signals from the RF antennas are fed to microwave mixers respectively. The mixers are driven by a local oscillator.
申请公布号 KR870000259(B1) 申请公布日期 1987.02.21
申请号 KR19800002598 申请日期 1980.07.01
申请人 GENERAL DYNAMICS CORP. 发明人 DURAND JR. CHAHES C.;HAWES JR.RALPH E.
分类号 F41G7/22;(IPC1-7):F41G7/22;F42B15/02 主分类号 F41G7/22
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