JOINED ANTIAIRCRAFT GUIDED MISSILE SYSTEM Russian patent published in 2006 - IPC F41H7/00 F41A23/42 

Abstract RU 2273815 C1

FIELD: armament, in particular, antiaircraft guided missile systems.

SUBSTANCE: the system is made in the form of a base vehicle that has two extreme sections and one central section suspended between them by means of an automatic coupling device for uncoupling of the extreme sections from the central one. The central section is provided with a target lighting and missile guidance radar. Installed on the extreme sections are launching-loading sets with doubling control panels of the antiaircraft guided missile launching system.

EFFECT: enhanced maneuverability of the system and reduced length of the column in the flight run.

2 dwg

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RU 2 273 815 C1

Authors

Anikonov Andrej Nikolaevich

Kovalev Vladimir Georgievich

Bulychev Oleg Fedorovich

Belokon' Sergej Petrovich

Radin Aleksandr Alekseevich

Rojanova Valentina Alekseevna

Dates

2006-04-10Published

2004-11-01Filed