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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Authors
Dates
2006-04-10—Published
2004-11-01—Filed