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AAir defence
Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile
BAir defence
small, lightweight, infrared homing surface-to-air missile in use
At a glance
ATILGAN PMSSlarger figure on 1 of 2
RIM-116 Rolling Airframe Missilelarger figure on 1 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source4.863 m (16.0 ft)[source]
Length
DisputedConfiguration
| Specification | ATILGAN PMSS | RIM-116 Rolling Airframe Missile |
|---|---|---|
| Type | Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile[source] | SAM -based CIWS[source] |
| Place of origin | Turkey[source] | Germany and United States[source] |
| In service | 2001–present[source] | 1992–present[source] |
| Used by | Turkish Armed Forces Turkish Naval Forces[source] |
missile
Single source2.79 m (9 ft 2 in) (missile)[source]
Length: 2.79 m (9 ft 2 in)[source]RIM-116 Rolling Airframe Missile · General characteristics · Length: 2.79 m (9 ft 2 in)
Length: 9.3 ft (2.83 m)[source]RIM-116 Rolling Airframe Missile · General characteristics · Length: 9.3 ft (2.83 m)
Length: 9.45 ft (2.88 m)[source]RIM-116 Rolling Airframe Missile · General characteristics · Length: 9.45 ft (2.88 m)
Block 1 missile
Single sourceBlock 2 missile
Single sourceDiameter
Disputed127 mm (5 in) (Block 1 missile) 159 mm (6.25 in) (Block 2 missile)[source]
Diameter: 127 mm (5.0 in)[source]RIM-116 Rolling Airframe Missile · General characteristics · Diameter: 127 mm (5.0 in)
Diameter: 5 in (12.70 cm)[source]RIM-116 Rolling Airframe Missile · General characteristics · Diameter: 5 in (12.70 cm)
Diameter: 6.25 in (15.88 cm)[source]RIM-116 Rolling Airframe Missile · General characteristics · Diameter: 6.25 in (15.88 cm)
Mass
Single source15.3 t (33,731 lb)[source]
launcher
Single sourcemissile
Single sourceWeight
Disputed5,777 kg (12,736 lb ) (launcher) 73.5 kilograms (162 lb 1 oz) (missile)[source]
Weight: 164 lb (74.4 kg)[source]RIM-116 Rolling Airframe Missile · General characteristics · Weight: 164 lb (74.4 kg)
Weight: 194.4 lb (88.2 kg)[source]RIM-116 Rolling Airframe Missile · General characteristics · Weight: 194.4 lb (88.2 kg)
(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; In excess of Mach 2 (
Single sourceMaximum; Maximum speed
Single sourceDetroit Diesel 6V53T, 6-cylinder diesel engine
Single sourceDetroit Diesel 6V53T, 6-cylinder diesel engine 205 kW (275 hp)[source]
Warhead weight
Single source11.3 kg (24 lb 15 oz)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
§ Operators[source] |
| Manufacturer | ROKETSAN and ASELSAN[source] | General Dynamics (now Raytheon) and Diehl Defence[source] |
|---|
| Produced | 2001–present[source] | 1985–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] | — |
|---|
| Designer | — | General Dynamics (now Raytheon ) and Diehl BGT Defence[source] |
|---|
| Designed | — | 1976[source] |
|---|
| Unit cost | — | US$998,000 (FY2014) US$905,330 (FY2021) (average)[source] |
|---|
| Variants | — | § Variants[source] |
|---|
| Warhead | — | Blast fragmentation warhead[source] |
|---|
| Engine | — | Hercules/Bermite Mk. 36 solid-fuel rocket[source] |
|---|
| Propellant | — | Solid[source] |
|---|
| Guidance system | — | Three modes: passive radio frequency/infrared homing, infrared only, or infrared dual mode enabled (radio frequency and infrared homing)[source] |
|---|
| Accuracy | — | Over 95%[source] |
|---|
| Launch platform | — | Mk 144 Guided Missile Launcher (GML) of the Mk 49 Guided Missile Launching System (GMLS)[source] |
|---|
| Role | — | small, lightweight, infrared homing surface-to-air missile in use[source] |
|---|
| Source measurement | — | The Rolling Airframe Missiles, together with the Mark 49 Guided Missile Launching System (GMLS) and support equipment, make up the RAM Mk 31 Guided Missile Weapon System (GMWS). The Mk-144 Guided Missile Launcher (GML) unit weighs 5,777 kilograms (12,736 lb) and stores 21 missiles. The original weapon cannot employ its own sensors prior to firing, so it must be integrated with a ship's combat system, which directs the launcher at targets. On U.S. ships, it is integrated with the AN/SWY-2 Ship Defense Surface Missile System (SDSMS) and Ship Self-Defense System (SSDS) Mk 1 or Mk 2-based combat systems. SeaRAM, a launcher variant equipped with independent sensors derived from the Vulcan Phalanx CIWS , is being installed on Independence-class littoral combat ships and certain Arleigh Burke -class destroyers .[source]RIM-116 Rolling Airframe Missile · Lead; only the objects and conditions stated in this passage The Block 2 (RIM-116C) is an upgraded version of the RAM missile aimed at more effectively countering more maneuverable anti-ship missiles through a four-axis independent control actuator system, increased rocket motor capability to 15.8 cm (6.25–inch) diameter, an improved passive radio frequency seeker and upgraded components of the infrared seeker, and advanced kinematics. On 8 May 2007, the U.S. Navy awarded Raytheon Missile Systems a $105 million development contract. Development was expected to be completed by December 2010. LRIP began in 2012.[source]RIM-116 Rolling Airframe Missile · Variants / Block 2; only the objects and conditions stated in this passage Length: 2.79 m (9 ft 2 in)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Diameter: 127 mm (5.0 in)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Fin span: 434 mm (1 ft 5.1 in)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Warhead: 11.3 kg (24.9 lb) blast fragmentation with 7.9 lb (3.6 kg) High-Explosive[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Launch weight: 73.5 kg (162 lb)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Range: 10 km (6.2 mi)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Length: 9.3 ft (2.83 m)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Diameter: 5 in (12.70 cm)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Wingspan: 17.5 in (44.45 cm)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Weight: 164 lb (74.4 kg)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Length: 9.45 ft (2.88 m)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Diameter: 6.25 in (15.88 cm)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Wingspan: 12.65 in (32.13 cm)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage Weight: 194.4 lb (88.2 kg)[source]RIM-116 Rolling Airframe Missile · General characteristics; only the objects and conditions stated in this passage |
|---|
| Launch weight | — | Launch weight: 73.5 kg (162 lb)[source]RIM-116 Rolling Airframe Missile · General characteristics · Launch weight: 73.5 kg (162 lb) |
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| Reported operators | — |
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In excess of Mach 2 (1,500 mph ; 2,500 km/h )[source]