
AAir defence
ATILGAN PMSS
Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile
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 1 of 3
MIM-23 Hawklarger figure on 2 of 3
Measured figures
Length
Single source4.863 m (16.0 ft)[source]
Length
Single sourceConfiguration
| Specification | ATILGAN PMSS | MIM-23 Hawk |
|---|---|---|
| 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] | United States[source] |
| In service | 2001–present[source] | August 1960 –present[source] |
| Used by | Turkish Armed Forces Turkish Naval Forces[source] | — |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
16 feet 8 inches (5.08 m)[source]
Wingspan
Single source3 feet 11 inches (1.19 m)[source]
(Basic), 3 (STC)
Single source2 (Basic), 3 (STC)[source]
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] |
Raytheon Company[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 | — | Cold War War of Attrition Chadian–Libyan War Iran–Iraq War Gulf War Second Libyan Civil War 2020 Turkish intervention in Libya Russo-Ukrainian War Russian invasion of Ukraine[source] |
|---|
| Warhead | — | 119 pounds (54 kg) blast fragmentation warhead[source] |
|---|
| Engine | — | solid-fuel rocket engine[source] |
|---|
| Flight ceiling | — | 65,000 feet (20,000 m)[source] |
|---|
| Guidance system | — | Semi-active radar homing[source] |
|---|
| Reported operators | — |
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