Credit
Антон Бородин · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Kh-22larger figure on 4 of 4
Measured figures
Length
Single source11.65 m (38.2 ft)[source]
Length
Single sourceConfiguration
| Specification | Kh-22 | Wan Chien |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Air-launched cruise missile Air-to-ground missile[source] |
| Place of origin | Soviet Union[source] | Taiwan[source] |
| In service | 1968-present[source] | 2011 – present[source] |
| Used by | Russia[source] | Republic of China Air Force[source] |
Wan Chienlarger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
350 cm (138 in)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Russo-Ukrainian War Russo-Ukrainian war[source] | — |
|---|
| Designer | MKB Raduga[source] | — |
|---|
| Unit cost | $1 million[source] | — |
|---|
| Produced | 1962[source] | — |
|---|
| Warhead | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] | 350kg of submunitions[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | Turbofan[source] |
|---|
| Propellant | Tonka-250 and IRFNA[source] | — |
|---|
| Flight ceiling | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] | — |
|---|
| Guidance system | Inertial guidance followed by terminal active radar homing[source] | GPS and inertial guidance[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | — |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | — |
|---|
| Manufacturer | MKB Raduga[source] | National Chung-Shan Institute of Science and Technology[source] |
|---|
| Reported operators |
| — |
|---|