Preparing your view.
AAir defence
Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile
At a glance
ATILGAN PMSSlarger figure on 0 of 1
S-200 missile system
Measured figures
Length
Single source4.863 m (16.0 ft)[source]
second stage only
Single sourceConfiguration
| Specification | ATILGAN PMSS | S-200 missile system |
|---|---|---|
| Type | Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile[source] | Strategic SAM system[source] |
| Place of origin | Turkey[source] | Soviet Union[source] |
| In service | 2001–present[source] | 1967–present[source] |
| Used by | Turkish Armed Forces Turkish Naval Forces[source] | See list of present and former operators |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
with boosters
Single source10,764 mm (35.315 ft) (with boosters) 10,452 mm (34.291 ft) (second stage only)[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; Mach 4.1
Single sourceMaximum; Maximum speed · source measurement 2
Single sourceDetroit Diesel 6V53T, 6-cylinder diesel engine
Single sourceDetroit Diesel 6V53T, 6-cylinder diesel engine 205 kW (275 hp)[source]
Warhead weight
Single source217 kg (478 lb)[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] | Almaz-Antey[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] | — |
|---|
| Wars | — | First Libyan Civil War Syrian civil war Russo-Ukrainian war[source] |
|---|
| Designer | — | KB-1 design bureau (system), GSKB Spetsmash (launcher)[source] |
|---|
| Designed | — | 1964[source] |
|---|
| Variants | — | S-200A, S-200V, S-200M, S-200VE, S-200D, S-200C[source] |
|---|
| Guidance system | — | Semi-active radar homing[source] |
|---|
| Warhead | — | Frag-HE[source] |
|---|
| Detonation mechanism | — | Proximity and command fusing[source] |
|---|
| Engine | — | Main: Dual-thrust liquid-fueled rocket engine Boosters: 4 solid-fueled strap-on rocket boosters[source] |
|---|
| Flight ceiling | — | 40,800 metres (133,900 ft)[source] |
|---|
| Boost time | — | 3–5.1 seconds[source] |
|---|
| Reported operators | — |
|
|---|
Maximum; Maximum speed · source measurement 3
Single source1,400 m/s (Mach 4.1; 5,000 km/h; 3,100 mph)[source]