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BAir defence
Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile
At a glance
Arrow (missile family)larger figure on 2 of 2
ATILGAN PMSSlarger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single sourcebooster section
Single sourceConfiguration
| Specification | Arrow (missile family) | ATILGAN PMSS |
|---|---|---|
| Type | Anti-ballistic missile[source] | Self-propelled anti-aircraft weapon Mobile air defense missile system Surface to air missile[source] |
| Place of origin | Israel United States[source] | Turkey[source] |
| In service | 2000–present[source] | 2001–present[source] |
| Used by | Israel[source] | Turkish Armed Forces Turkish Naval Forces |
kill vehicle section
Single sourcesustainer section
Single source6.8 m (22 ft) – 7 m (23 ft) 3.45 m (11.3 ft) – booster section 0.75 m (2.5 ft) – sustainer section 2.75 m (9.0 ft) – kill vehicle section[source]
Length
Single source4.863 m (16.0 ft)[source]
2nd stage
Single sourceBy stage 1st stage
Single sourceBy stage: 800 mm (31 in) – 1st stage 500 mm (20 in) – 2nd stage[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]
Warhead weight
Single source150 kg (330 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | March 2017 Israel–Syria incident Gaza war 2024 Israel–Iran conflict Iran–Israel war[source] | — |
|---|
| Designer | Israel Aerospace Industries , Boeing[source] | — |
|---|
| Designed | 1994–present[source] | — |
|---|
| Manufacturer | Israel Aerospace Industries , Boeing Defense, Space & Security[source] | ROKETSAN and ASELSAN[source] |
|---|
| Unit cost | US$3 million (as of 2003 )[source] | — |
|---|
| Produced | 1994–present[source] | 2001–present[source] |
|---|
| Warhead | Directed high explosive fragmentation[source] | — |
|---|
| Detonation mechanism | Proximity fuze[source] | — |
|---|
| Engine | Two-stage[source] | — |
|---|
| Propellant | Solid propellant[source] | — |
|---|
| Flight ceiling | Endo-exo atmospheric[source] | — |
|---|
| Guidance system | Dual mode: passive infrared seeker and active radar seeker[source] | — |
|---|
| Steering system | Thrust vectoring and four aerodynamic control moving fins[source] | — |
|---|
| Accuracy | Within 4 m (13 ft) of the target[source] | — |
|---|
| Launch platform | Six canisters per trailer-mounted erector–launcher[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] |
|---|