FORCETALLY
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At a glance
Hsiung Feng IIElarger figure on 0 of 3
Kh-22larger figure on 3 of 3
Measured figures
Length
Single source600 cm (236 in)[source]
Length
Single sourceConfiguration
| Specification | Hsiung Feng IIE | Kh-22 |
|---|---|---|
| Type | Land-attack cruise missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | Taiwan[source] | Soviet Union[source] |
| In service | 2011 – present[source] | 1968-present[source] |
| Used by | Republic of China (Taiwan) Armed Forces[source] | Russia |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
11.65 m (38.2 ft)[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]
Operational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer | National Chung-Shan Institute of Science and Technology[source] | MKB Raduga[source] |
|---|
| Unit cost | ~3m USD (2003)[source] | $1 million[source] |
|---|
| Produced | ~300 (2012), in production[source] | 1962[source] |
|---|
| Warhead | 220 kg (490 lb)[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Engine | turbofan with solid rocket booster[source] | R-201 liquid-fuel rocket[source] |
|---|
| Guidance system | GPS , TERCOM , and inertial guidance with automatic target recognition for terminal guidance[source] | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Accuracy | 10 to 15 m[source] | >300 ft (91 m) (CEP)[source] |
|---|
| Wars | — | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Designer | — | MKB Raduga[source] |
|---|
| Propellant | — | Tonka-250 and IRFNA[source] |
|---|
| Flight ceiling | — | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
|---|
| Launch platform | — | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| Reported operators | — |
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