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 dwg
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Authors
Dates
1998-08-20—Published
1997-05-29—Filed