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AAir defence
Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile
At a glance
ATILGAN PMSSlarger figure on 1 of 3
HQ-12larger figure on 2 of 3
Measured figures
Length
Single source4.863 m (16.0 ft)[source]
Length
Single sourceConfiguration
| Specification | ATILGAN PMSS | HQ-12 |
|---|---|---|
| Type | Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile[source] | Surface-to-air missile[source] |
| Place of origin | Turkey[source] | China[source] |
| In service | 2001–present[source] | 2007–present[source] |
| Used by | Turkish Armed Forces Turkish Naval Forces[source] | See § Operators |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
5,644 mm (222.2 in)[source]
(Basic), 3 (STC)
Single source2 (Basic), 3 (STC)[source]
Maximum; on land
Single sourceMaximum; swimming
Single source67.6 km/h (36.5 kn; 42.0 mph) on land 5.8 km/h (3.1 kn; 3.6 mph) swimming[source]
Maximum; KS-1 · Speed
Single sourceMaximum; Maximum speed
Single source1,200 m/s (3,900 ft/s)
Detroit Diesel 6V53T, 6-cylinder diesel engine
Single sourceDetroit Diesel 6V53T, 6-cylinder diesel engine 205 kW (275 hp)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer | ROKETSAN and ASELSAN[source] | — |
|---|
| Produced | 2001–present[source] | — |
|---|
| No. built | 100+[source] | — |
|---|
| Main armament | 4 or 8 FIM-92 Stinger missiles[source] | — |
|---|
| Secondary armament | 1x 12.7 mm (0.500 in) automatic machine gun[source] | — |
|---|
| Payload capacity | 8 ready-to-fire Stinger missiles[source] | — |
|---|
| Suspension | torsion bar, 5 road wheels[source] | — |
|---|
| Warhead | — | 100 kg (220 lb)[source] |
|---|
| Detonation mechanism | — | Impact/proximity[source] |
|---|
| Engine | — | Rocket motor[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight altitude | — | 500 m (1,600 ft) to 25 km (16 mi)[source] |
|---|
| Guidance system | — | Semi-active radar homing / radio-command guidance[source] |
|---|
| Launch platform | — | 6x6[source] |
|---|
1,200 m/s (2,684 mph, 4,320 km/h)[source]