FIELD: military equipment
SUBSTANCE: invention relates to military equipment, mainly to means of combating harsh targets, for example, thick-walled protective structures and / or runways. The warhead includes front and rear blocks with their own explosive charges and bottom fuses, and the front block is thick–walled and sub-caliber relative to the rear with a penetrating type head, and the rear is thin-walled. The blocks are made autonomous and connected coaxially by a low-strength fastening unit, and the head of the front block is made in the form of two conjugated cones with a total length of 2.4-5.0 of its caliber with a solution angle of the front cone equal to 100-180 degrees and a diameter of its base of 0.45-0.90 of the caliber of this block, and the rear block - it consists of one and/or more independent subunits in the form of cylindrical cups, each of which is equipped with its own explosive charge and bottom fuse, and the caliber of the subsequent block or subunit is equal to 1-2 calibers of the previous one, and the warhead itself is equipped with a device for its delivery to the target in the form of a solid-fuel rocket engine, made with the possibility of axial rotation and connected to the warhead by an attachment unit with a weakened cross-section.
EFFECT: creating a design that allows for reliable delivery of a warhead to a given point and completing the task at an angle of 28-90 degrees to the target surface without ricocheting.
4 cl, 3 dwg
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Authors
Dates
2025-02-11—Published
2006-09-21—Filed