
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
Measured figures
(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; R440 Mach 2.3
Single sourceMaximum; VT-1 Mach 3.6
Single sourceDetroit 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.
Configuration
| Specification | ATILGAN PMSS | Crotale (missile) |
|---|---|---|
| Type | Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile[source] | Surface-to-air missile system[source] |
| Place of origin | Turkey[source] | France[source] |
| In service | 2001–present[source] | — |
| Used by | Turkish Armed Forces Turkish Naval Forces[source] | See Operators[source] |
| Manufacturer | ROKETSAN and ASELSAN[source] | Thales Group Samsung Group[source] |
| Produced | 2001–present[source] | Early 1970s[source] |
| No. built | 100+[source] | 6,600 missiles (R440)[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 | — | Chadian-Libyan conflict South African Border War Russian invasion of Ukraine[source] |
| Designed | — | Late 1960s[source] |
| Warhead | — | forward-directed blast warhead (R.440 and R.460) or blast-fragmentation warhead (VT-1)[source] |
| Detonation mechanism | — | infrared fuse, converted to RF fuse in later models.[source] |
| Engine | — | Lens 3 solid-fuel boost-glide (R.440)[source] |
| Flight ceiling | — | VT-1: 6,000 m Mk3: 9,000 m[source] |
| Guidance system | — | Automatic command to line of sight[source] |
| Steering system | — | Canard and tail axis control[source] |
| Launch platform | — | Mobile Launcher, Naval Launch[source] |
R440: 800 m/s (Mach 2.3) VT-1: 1250 m/s (Mach 3.6)[source]