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Measured figures
Configuration
| Specification | Abu Mahdi (missile) | Ra'ad-II |
|---|---|---|
| Speed | — | ≤0.8 Mach. (980 km/h (610 mph))[source]Source text · numeric interpretation needs review |
| Type | Cruise missile[source] | ALCM[source] |
| Place of origin | Iran[source] | Pakistan[source] |
| In service | 20 August 2020[source] | 2020 –Present[source] |
Diameter
Single source0.50 m (20 in)[source]
Warhead weight
Single source450 kg (990 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by | Iran[source] | Pakistan Air Force Air Force Strategic Command[source] |
|---|
| Warhead | High Explosive[source] | ICM / HE / NE[source] |
|---|
| Designer | — | National Engineering & Scientific Commission (Guidance/controls) Air Weapons Complex (Warhead design/assembly)[source] |
|---|
| Designed | — | 2007–2019[source] |
|---|
| Manufacturer | — | Air Weapons Complex[source] |
|---|
| Developed into | — | Taimoor[source] |
|---|
| Blast yield | — | 5 kilotons of TNT (21 TJ)—12 kilotons of TNT (50 TJ)[source] |
|---|
| Engine | — | Turbojet[source] |
|---|
| Payload capacity | — | ≤450 kg (990 lb)[source] |
|---|
| Flight altitude | — | Terrain-following[source] |
|---|
| Guidance system | — | Inertial , Terminal[source] |
|---|
| Accuracy | — | 3.0 m (9.8 ft) CEP[source] |
|---|
| Launch platform | — | JF-17A/B , Mirage-IIIR , Mirage-VR[source] |
|---|
| Transport | — | Combat aircraft[source] |
|---|
| Role | — | standoff and an air-launched cruise missile (ALCM)[source] |
|---|