FIELD: weapons and ammunition.
SUBSTANCE: proposed simulator comprises launching tube, starting motor with electric contacts. Launching tube accommodates rocket model. Receiver, launching mechanism connector, mechanical sight front and rear posts are arranged at launching tube. Launching tube is equipped with starting motor electric connector connected electrically with launching mechanism connector. Note here that simulator exploits optics-electronic receiver. Besides, it incorporates signal digital processing unit which, combined with said receiver, acts a self-guidance head. Receiver output is connected to signal digital processing unit input. Signal digital processing unit output is electrically connected with launching mechanism connector. Rocket model represents inertial component. Foresight is secured at mechanical sight front post while backsight is secured at rear post along with light data indicator electrically connected with launching mechanism connector. Note here that sight observing line is parallel with receiver optical axis.
EFFECT: efficient simulator of portable antiaircraft rocket launcher, lower production costs.
2 cl, 1 dwg
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