SELF-PROPELLED ROCKET LAUNCHER

WIPO Patent Application WO/2019/083395

A3

The utility model relates to the field of military hardware and can be used as a primary means of combat in medium-range surface-to-air missile systems. A self-propelled rocket launcher comprises a self-propelled chassis on which are disposed a launcher with a set of surface-to-air guided missiles, an electrohydraulic servo drive, a radar station, a digital computing system, an encoded data transmission system, an optoelectronic system with a power drive, and a passive unit. The utility model provides timely deactivation of the radar transmitter and allows "spiral" scanning of an airspace using an optical lens of the optoelectronic system upon detection of a target in passive mode in external target designation mode. The technical result is that of keeping the location of the self-propelled rocket launcher concealed during target designation from an external command centre.

SAVINOV ANDREJ LEONIDOVICH (RU)
BASALOV STANISLAV ALEKSEEVICH (RU)
LAPIN VYACHESLAV VIKTOROVICH (RU)
VORONTSOV VLADIMIR ALEKSEEVICH (RU)
KUZNETSOV VYACHESLAV PETROVICH (RU)
GORNOSTAEV VLADIMIR MIKHAJLOVICH (RU)
BELYJ YURIJ IVANOVICH (RU)
FEDOROV STANISLAV VLADIMIROVICH (RU)
MONIN ALEKSANDR EVGENEVICH (RU)
VASILEV ANATOLIJ FEDOROVICH (RU)
LARIONOV YURIJ PETROVICH (RU)
SHAROV VLADIMIR SERGEEVICH (RU)
MAKEEV ANATOLIJ VASILEVICH (RU)

PCT/RU2017/000973

June 06, 2019

December 26, 2017

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JOINT STOCK COMPANY «AIR AND SPACE DEFENCE CORP «ALMAZ ANTEY» (RU)
JOINT STOCK COMPANY «ULYANOVSK MECH PLANT» (RU)

F41F3/04; F41G7/20

RU89217U1	2009-11-27
RU2230459C2	2004-06-20

MAZUR, Natalya Zinovevna et al. (RU)

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