ROCKET Russian patent published in 2007 - IPC F42B12/22 

FIELD: armament.

SUBSTANCE: the rocket has an elongated with a nose fuze, including a body with a spherical head filled with a fluid detonating mixture and a cross diaphragm fastened on it, axial detonator and a jet solid-propellant engine. The rocket is provided with carrier shells and a disk membrane made of a set of leaf springs aligned on the screening cap of the axial detonator lug provided with a propellant charge, an ignition pyrotechnical composition is coaxially positioned inside the propellant charge. The elongated warhead with the nose fuze is installed on one of the shells, and the spherical head resting on the disk membrane is fastened on the other shell. The spherical head is made thin-walled and filled with a condensed explosive. From the inside the body is made channeled.

EFFECT: enhanced power of the rocket.

2 cl, 4 dwg