GUIDED MISSILE Russian patent published in 2009 - IPC F42B12/18 

FIELD: weapons and ammunition.

SUBSTANCE: missile incorporates leading cumulative charge (LCC), steering drive unit (SDU), main explosive part (EP), pipe attached the SDU casing and gas-generator pyrotechnical mechanism of pulling out the pipe together with SDU and LCC. The pipe can move and be locked relative to the main EP casing. The LCC casing is arranged coaxial to SDU casing inside the latter on disk-like base making together with the outer fairing the SDU. The SDU assembly units and parts are mounted the LCC casing. The gas-generator pyrotechnical mechanism of pulling out mechanism represents a circular power cylinder with circular piston rigidly fixed on the EP casing and an operating chamber formed by the disk-like base rear wall and cylindrical sleeve outer surface, the sleeve being arranged on the disk-like base rear wall. Gas generator is fitted on the disk-like base at the seat communicating, via appropriate channels, with the circular power cylinder operating chamber.

EFFECT: higher hitting efficiency of dual explosive part of guided missile, utilisation of "duck' aerodynamic configuration.

3 dwg