GUIDED ANTI-AIRCRAFT MISSILE Russian patent published in 2004 - IPC

FIELD: rocketry, applicable, in particular, in portable anti-aircraft missile complexes for destruction of low-altitude aircraft and helicopters. SUBSTANCE: the missile has an engine with a charge of solid propellant in the body, warhead and a fuse. The charge of solid propellant is made of a detonationable composition. The solid propellant blast attachment point is positioned between the engine body and the warhead, it represents a charge-detonator of explosive installed on the end face of the engine body, and a detonation transmission unit. One end of the detonation transmission unit is engageable with the warhead, and the other - with the charge-detonator. The charge-detonator and the detonation transmission unit may be manufactured of phlegmatized octogen. The charge-detonator may be made in the form of a cylinder with a diameter of not less than one and a height of not less than 0.3 of the critical diameter of detonation of solid propellant. The detonation transmission unit may have the shape of contain within 10 to 25 mass percent of hecogen. EFFECT: enhanced destructive defect of the missile. 2 cl, 2 dwg, 1 tbl