FIELD: armament.
SUBSTANCE: the mechanism of missile retaining in the launching container has a split spring ring and a multi-nozzle rocket engine with an installed circular stepped insert of a variable diameter. End-cap-pistons are installed in each nozzle of the nozzle unit. The split spring ring is made for installation in the ring-shaped cavity formed by the circular groove on the container and the outer circular groove on the engine. The circular stepped insert of a variable diameter is positioned for a rest on it of the installed rear cover before the ring lock is latched.
EFFECT: provided reliable retaining of the missile in the launching container, reduced impulse pressure, which makes it possible to launch the missile from hands.
3 cl, 5 dwg
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