FIELD: military engineering.
SUBSTANCE: device has missile warhead having a leading cumulative charge and onboard equipment provided with electric launching and control circuits are connected to ground control means. The electric launching circuits and controlled electric circuits are connected to the container via umbilical connector. Ring-shaped socket of the umbilical connector is arranged around the leading cumulative charge. It is connected to the electric rocket missile launching and control circuits and is snapped together with the umbilical connector plug-and-socket that is mounted on the internal side of frontal container cover and electrically connected to the launching and control plug-and-sockets sealed from container outside. The control plug is mounted on the external side of frontal container cover and sealed with plug.
EFFECT: improved rocket missile reliability.
1 dwg
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