CLUSTER NOSE CONE OF SPIN-STABILIZED MISSILE Russian patent published in 2007 - IPC F42B12/58 

FIELD: rocketry, in particular, cluster nose cones of spin-stabilized missile.

SUBSTANCE: the cluster nose cone has a body with tubular sections positioned along it. Cylinder-shaped fighting components are positioned in the tubular sections. One of the sections is provided with longitudinal thrust surfaces and positioned in the axis of missile spinning. The peripheral sections are positioned lengthwise by equal groups between the thrust surfaces of the central section. The diameter of the sections makes up 0.2 to 0.3 caliber of the cluster nose cone. The section length-to-fighting component length ratio is within 5 to 8.

EFFECT: enhanced efficiency of target destruction at the expense of uniformity of dispersion of the fighting components on the terrain.

3 dwg