Credit
Антон Бородин · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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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 | YJ-83 |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Anti-ship cruise missile[source] |
| Place of origin | Soviet Union[source] | China[source] |
| In service | 1968-present[source] | 1998–present[source] |
| Used by | Russia[source] | People's Liberation Army Navy[source] |
YJ-83larger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
6.38 metres (20.9 ft)[source]
Operational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Operational; C-802
Single sourceOperational; C-802A
Single sourceOperational; YJ-83KH
Single sourceOperational; YJ-83, YJ-83K
Single source180 km (YJ-83, YJ-83K) 230 km (YJ-83KH) 120 km (C-802) 180 km (C-802A)[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] | 190 kg high-explosive fragmentation (YJ-83) 165 kg high-explosive, semi-armour piercing (YJ-83K)[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | CTJ-2 turbojet[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] | Inertial navigation / active radar homing or imaging-infrared (IIR) terminal guidance[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | — |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | Surface and air launched[source] |
|---|
| Manufacturer | MKB Raduga[source] | China Aerospace Science and Industry Corporation[source] |
|---|
| Flight altitude | — | 20-30 m (cruise) 5-7 m (terminal)[source] |
|---|
| Reported operators |
| — |
|---|