发明名称 METHOD FOR FIRING THE GUIDED MISSILE AND GUIDED MISSILE
摘要 FIELD: missile armament. SUBSTANCE: method of firing the guided missile with side nozzles and elements of optical communication with control panel consists in missile control from control panel with simultaneous supply to zone behind the missile bottom part of optically transparent gas. Installed on missile with side nozzles of jet engine and elements of optical communication on its rear end is source of optically transparent gas. Gas source is connected through channel with the rear end of missile. EFFECT: higher reliability and efficiency of missile control. 4 cl, 2 dwgn
申请公布号 RU2117908(C1) 申请公布日期 1998.08.20
申请号 RU19970108991 申请日期 1997.05.29
申请人 KONSTRUKTORSKOE BJURO PRIBOROSTROENIJA 发明人 KUZNETSOV JU.M.;KRASEN'KOV V.N.;ORLOV V.V.;TELYSHEVA E.A.;CHUBUNOV V.A.
分类号 F42B15/00;(IPC1-7):F42B15/00 主分类号 F42B15/00
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