发明名称 Rolling dual mode missile
摘要 In a rolling missile a seeker system which is responsive to two forms of energy emanating from a target. The system has the capability to switch between guidance modes during its path towards its intended target.
申请公布号 US4264907(A) 申请公布日期 1981.04.28
申请号 US19680722104 申请日期 1968.04.17
申请人 GENERAL DYNAMICS CORPORATION, POMONA DIVISION 发明人 DURAND, JR., CHARLES C.;HAWES, JR., RALPH E.
分类号 F41G7/22;G01S13/86;G05D1/10;(IPC1-7):F41G7/00 主分类号 F41G7/22
代理机构 代理人
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