FIELD: military equipment.
SUBSTANCE: element contains a body with a warhead, a rotating parachute with a pole hole, with retractable spring-loaded brake flaps perpendicular to its longitudinal axis inside the element body. Contains an autonomous guidance system that includes, at a minimum, interconnected motion controller and target coordinator of the self-targeting battle element. In the lower part of the body, two rocket solid fuel engines are configured to rock with a possibility of step-by-step thrust control, and the controls for their operation are associated with an autonomous guidance system via the motion controller. The longitudinal axis of one of these engines is parallel to the longitudinal axis of the self-targeting battle element, and the longitudinal axis of the other engine is perpendicular to the longitudinal axis of the self-targeting battle element. The parachute is installed with a possibility of undocking from the body upon a command of the motion controller.
EFFECT: changing of the battle element trajectory to ensure the closest possible approach to the target.
3 dwg
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Authors
Dates
2018-04-28—Published
2016-05-24—Filed