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Measured figures
booster section
Single sourcekill vehicle section
Single sourceConfiguration
| Specification | Arrow (missile family) | Bavar-373 |
|---|---|---|
| Speed | Arrow 2: Mach 9, means 3 km/s (1.9 mi/s), Arrow 3: classified, mach 12-17[source] | — |
| Type | Anti-ballistic missile[source] | Mobile long range surface-to-air missile[source] |
| Place of origin | Israel United States[source] | Iran[source] |
| In service | 2000–present[source] | August 2019[source] |
Length
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]
2nd stage
Single sourceBy stage 1st stage
Single sourceBy stage: 800 mm (31 in) – 1st stage 500 mm (20 in) – 2nd stage[source]
"missile itself"
Single sourceofficially
Single sourcesealed canister
Single source1,300 kg (2,900 lb) – "missile itself" 2,800 kg (6,200 lb) – officially 3,500 kg (7,700 lb) – sealed canister[source]
Operational; Operational range
Single source90 km (56 mi) – 150 km (93 mi)[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.
| Used by | Israel[source] | See § Operators[source] |
|---|
| 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] | Iranian Defence Ministry[source] |
|---|
| Unit cost | US$3 million (as of 2003 )[source] | — |
|---|
| Produced | 1994–present[source] | 2014–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] | — |
|---|
| Source measurement | — | Bavar-373 utilizes Sayyad-4 missiles, which are contained in two rectangular launch canisters. No formal information was given about this missile, but it appears from news photos that Sayyad-4 is similar to Sayyad-3 in wings and control surfaces; however, it varies slightly in frontal shape.[source]Bavar-373 · Design; only the objects and conditions stated in this passage Bavar-373 uses a phased array radar for tracking aerodynamic targets and ballistic missiles in medium to long ranges, mounted on the ZAFAR heavy truck. Iran claims that it can track up to 200 targets simultaneously.[source]Bavar-373 · Design; only the objects and conditions stated in this passage |
|---|
| Reported operators | — |
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