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At a glance
Paveh cruise missilelarger figure on 1 of 1
Sea Skualarger figure on 0 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Configuration
| Specification | Paveh cruise missile | Sea Skua |
|---|---|---|
| Speed | — | Mach 1+[source] |
| Type | Strategic cruise missile system[source] | Air-to-surface missile , anti-ship missile[source] |
| In service | 2023 (Unveiled)[source] | 1982[source] |
| Used by | Iran Islamic Resistance in Iraq Houthi movement Hezbollah[source] | See operators[source] |
Wingspan
Single source0.72 m[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Gaza war[source] | Falklands War Gulf War[source] |
|---|
| Manufacturer | Iran ( Islamic Republic of Iran Navy )[source] | British Aircraft Corporation (1972–1977) BAe Dynamics (1977–1999) MBDA (UK) Ltd (since 1999)[source] |
|---|
| Engine | Turbo-jet engine[source] | Solid fuel booster / solid fuel sustainer[source] |
|---|
| Guidance system | A smart missile that can change targets mid-mission[source] | Semi-active radar homing[source] |
|---|
| Role | Iranian long-range surface-to-surface cruise missile[source] | — |
|---|
| National origin | Iran[source] | — |
|---|
| Source measurement | Paveh is a part of the Soumar cruise missile family, which was unveiled in 2015 with the first missile of the family being the Soumar which had a range of 700 km.[source]Paveh cruise missile · Development; only the objects and conditions stated in this passage On 2 February 2019, Iran unveiled the Hoveyzah Cruise Missile , a surface-to-surface missile with a claimed range of more than 1,350 kilometers.[source]Paveh cruise missile · Development; only the objects and conditions stated in this passage The missile has a range of 1,650 km (1,030 mi).[source]Paveh cruise missile · Design; only the objects and conditions stated in this passage | — |
|---|
| Place of origin | — | United Kingdom[source] |
|---|
| Designer | — | British Aircraft Corporation[source] |
|---|
| Designed | — | 1972[source] |
|---|
| Produced | — | 1975[source] |
|---|
| Warhead | — | 30 kg semi armour piercing, 9 kg RDX[source] |
|---|
| Detonation mechanism | — | Impact fuze, delayed detonation[source] |
|---|
| Steering system | — | Control surfaces[source] |
|---|
| Launch platform | — | Westland Lynx, Combattante BR-42 FAC[source] |
|---|