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Measured figures
Configuration
| Specification | Abu Mahdi (missile) | SSM-700K C-Star |
|---|---|---|
| Type | Cruise missile[source] | Anti-ship missile[source] |
| Place of origin | Iran[source] | South Korea[source] |
| In service | 20 August 2020[source] | 2006–present[source] |
| Used by | Iran[source] |
Diameter
Single source0.34 m[source]
Maximum; Mach 0.95
Single source1,162.8 km/h (Mach 0.95)[source]
Operational; >
Single source>180 kilometers (110 mi)[source]
Warhead weight
Single source250 kg[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
See § Users[source] |
| Warhead | High Explosive[source] | — |
|---|
| Designer | — | Agency for Defense Development LIG Nex1 Hanwha Techwin[source] |
|---|
| Designed | — | 1996–2003[source] |
|---|
| Manufacturer | — | LIG Nex1 Samsung/Hanwha Techwin[source] |
|---|
| Unit cost | — | ₩ 2,000,000,000 (US$1.75 million)[source] |
|---|
| Produced | — | 2004–present[source] |
|---|
| Detonation mechanism | — | Impact fuze[source] |
|---|
| Engine | — | Hanwha Techwin SS-760K (later SSE-750K) turbojet[source] |
|---|
| Flight altitude | — | Sea-skimming[source] |
|---|
| Guidance system | — | GPS -aided inertial navigation (mid-course phase) Active radar homing (terminal phase)[source] |
|---|
| Reported operators | — |
|
|---|