Launcher unit |
The main component of the towed PL-9C station is the launcher unit, which is carried on a two-wheeled A-frame trailer. When in the firing position, the wheels are removed from the ground and the trailer is stabilised on four adjustable outriggers. The launcher consists of a large rectangular unit carrying two missiles on each side ready to be fire.
|
Missile |
The missile is fitted with a cryogenic liquid nitrogen gas-cooled IR seeker capable of +/-40 degree off boresight angles. Flight control is by long span pointed delta fins at the front of the missile with Sidewinder-type slipstream driven rollerons on the aft tail fin surfaces to prevent roll and so enhance the operation of the guidance system. The missile has a maximum effective range of 35 km and an altitude limit of 6.5 km. The single-shot hit probability for a single missile launch at an approaching target is 90%.
|
Radar and control components. |
The PL9C launcher unit is associated to target acquisition and radar and electro-optical director mounted on a 6x6 WZ551 armoured vehicle personnel carrier or to the AF902 fire control radar which is equipped with an X-Band search radar, a C-Band Search/Tracking radar, a Ka-Band tracking radar and electro-optical system with TV tracking range, IR tracking range and laser range finder.
|
Mobility |
The mobile PL9C SHORAD is normally towed by a 4x4 light tactical vehicle or military truck.
|
Operations |
The launcher unit is supported by a range of truck-mounted ground equipment for maintenance and missile testing.
|
|
Specifications |
Back to top |
Type
|
Short range ground-to-air missile system
|
Country users
|
China a a a
|
Designer Country
|
China
|
Weight launcher unit
|
? kg a
|
Dimensions launcher unit
|
Length, ? m; Width, ? m; Height, ? m
|
|
Type of engaged targets
|
helicopter, fighter aircraft, cruise missile
|
Missile
|
Weight: 115 kg Weight Warhead: 12 kg Warhead type : HE Flight speed: Mach 2.1
|
Range
|
Range: 500 m - 22,000 m
|
Guidance system
|
infrared-homing seeker head unit, which utilises proportional navigation guidance techniques.
|
Missile dimensions
|
Length: 2.9 m; Diameter: 0.157 m; Wingspan: 0.65m
|
|
|
|