FIELD: weapons and ammunition.
SUBSTANCE: group of inventions relates to armament, namely to grenade launcher systems of side impact. Grenade of a grenade launcher complex contains a charge of an explosive, a fragmentation element, a rocket engine, aerodynamic stabilizers and a timer. According to a first embodiment the grenade fragmentation element is located on one side of the explosive charge placed in the cylindrical body with the possibility of rotating separately or together with the fragmentation element. According to a second embodiment the grenade fragmentation element is located on one side of the explosive charge, and the launcher grenade contains a gyroscope axis of which is perpendicular to the longitudinal axis of the grenade, contains power supply, electronic stabilization system, executive steering machines and aerodynamic steering wheels.
EFFECT: increase in the damaging effect of the grenade in one direction perpendicular to the direction of flight is achieved.
7 cl, 4 dwg
Authors
Dates
2018-06-08—Published
2017-02-02—Filed