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

FIELD: weapons and ammunition.

SUBSTANCE: guided missile comprises fair, tandem combat part comprising leading shaped charge (LSC), main combat part and head contact device arranged on missile nose fair extending with the help of pyro mechanism with gas generator. Aforesaid pyro mechanism represents a cylindrical base arranged on LSC casing and furnished with dead circular clearance relative to LSC casing and fitted in circular clearance of hollow piston representing a thin-wall cylinder jointed to nose fair. Sealing elements are fitted along the cylindrical base faces. Spring ring is arranged on front-end face of the said cylindrical base to lock piston in pulled-out position. Aforesaid cylindrical base, piston with nose fair, casing and LSC funnel form a closed chamber communicated with gas generator fastened at the cylindrical base rear end face.

EFFECT: higher combat efficiency.

2 cl, 2 dwg