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Measured figures
Configuration
| Specification | Abu Mahdi (missile) | Hsiung Feng IIE |
|---|---|---|
| Type | Cruise missile[source] | Land-attack cruise missile[source] |
| Place of origin | Iran[source] | Taiwan[source] |
| In service | 20 August 2020[source] | 2011 – present[source] |
| Used by | Iran[source] |
Diameter
Single source510 mm (20 in)[source]
Maximum; Mach 0.75 - 0.85
Single source( Mach 0.75 - 0.85) 919–1,041 km/h (571–647 mph)[source]
Operational; >
Single sourceOperational; for Hsiung Sheng
Single sourceOperational; Various reported ranges from to >
Single sourceVarious reported ranges from 600 km to >2,000km >1200 km for Hsiung Sheng[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Republic of China (Taiwan) Armed Forces[source] |
| Warhead | High Explosive[source] | 220 kg (490 lb)[source] |
|---|
| Manufacturer | — | National Chung-Shan Institute of Science and Technology[source] |
|---|
| Unit cost | — | ~3m USD (2003)[source] |
|---|
| Produced | — | ~300 (2012), in production[source] |
|---|
| Engine | — | turbofan with solid rocket booster[source] |
|---|
| Guidance system | — | GPS , TERCOM , and inertial guidance with automatic target recognition for terminal guidance[source] |
|---|
| Accuracy | — | 10 to 15 m[source] |
|---|