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Measured figures
C-704
Single source3.284 m (10.77 ft) (C-704)[source]
Configuration
| Specification | Abu Mahdi (missile) | C-704 |
|---|---|---|
| Speed | — | Mach 0.8[source] |
| Type | Cruise missile[source] | Anti-ship / air-to-surface[source] |
| Place of origin | Iran[source] | China[source] |
| In service | 20 August 2020[source] | Prior to 2006 – present[source] |
extended; C-704
Single sourcefolded; C-704
Single source480 mm (19 in) (folded; C-704) 1,018 mm (3.340 ft) (extended; C-704)[source]
C-704
Single source28 cm (11 in) (C-704)[source]
C-704
Single source360 kg (790 lb) (C-704)[source]
Operational; C-704
Single sourceOperational; C-705; with booster
Single sourceOperational; C-705; without booster
Single source38 km (24 mi; 21 nmi) (C-704) 75 km (47 mi; 40 nmi) (C-705; without booster) 170 km (110 mi; 92 nmi) (C-705; with booster)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Used by | Iran[source] | China Bangladesh Egypt Indonesia Iran Pakistan[source] |
|---|
| Warhead | High Explosive[source] | 130 kg (290 lb) warhead (C-704) 110–130 kg (240–290 lb) warhead (C-705)[source] |
|---|
| Manufacturer | — | China Aerospace Science and Industry Corporation (CASIC)[source] |
|---|
| Produced | — | Prior to 2006[source] |
|---|
| Detonation mechanism | — | Semi-armor-piercing[source] |
|---|
| Engine | — | Rocket motor (C-704) Turbojet (C-705)[source] |
|---|
| Propellant | — | Solid fuel[source] |
|---|
| Flight altitude | — | 15–20 m (49–66 ft) (cruising; C-704) 5–7 m (16–23 ft) (terminal strike; C-704) 12.15 m (39.9 ft) (cruising; C-705)[source] |
|---|
| Guidance system | — | Active radar homing / imaging infrared homing / TV[source] |
|---|
| Launch platform | — | Air and surface[source] |
|---|