FIELD: military equipment.
SUBSTANCE: motorized missile system contains a carrier that includes the operator's work area, remote control and combat compartment with a launching machine (LM). The LM contains guidance mechanisms, a aiming sight-guidance unit, a mechanism for LM changeover to fire and travel positions. The mechanism for LM changeover is rigidly fixed to the traverse platform by a arrester catch including a base with a guide in which the right and left sliders are installed and with an hole in which the shaft with the screw is arranged for longitudinal movement, an electric actuator, a sensor of the released and latched position of the sliders, the right and left thrusts. The frame is provided with upper and lower supports with grooves concentrically arranged relative to the axis of the traverse platform. The rods are pivotally connected at one end to the upper part of the shaft, and at the other - to the right and left sliders.
EFFECT: creation of a motorized missile system with small mass-size characteristics and a reduced time of the complex changeover to fire and travel positions.
3 cl, 5 dwg
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Authors
Dates
2017-08-01—Published
2016-08-03—Filed