

Preparing your view.


BCruise & anti-ship missiles
Cruise missile Air-launched cruise missile Submarine-launched cruise missile Anti-ship missile Surface-to-surface missile Land-attack missile
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 | P-800 Oniks |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Cruise missile Air-launched cruise missile Submarine-launched cruise missile Anti-ship missile Surface-to-surface missile Land-attack missile[source] |
| Place of origin | Soviet Union[source] | Soviet Union / Russia[source] |
| In service | 1968-present[source] | 2002–present[source] |
| Used by | Russia[source] | See Operators |
P-800 Onikslarger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
8.9 m (29.2 ft)[source]
Operational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Operational; depending on altitude ( Yakhont export version)
Single sourceOperational; Oniks-M version for Russia
Single sourceOperational; Oniks version for Russia
Single source600 km (370 mi; 320 nmi) ( Oniks version for Russia) 800 km (500 mi; 430 nmi) ( Oniks-M version for Russia) 120 to 300 km (75 to 186 mi; 65 to 162 nmi) depending on altitude ( Yakhont export version)[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] | Syrian Civil War Russo-Ukrainian war[source] |
|---|
| Designer | MKB Raduga[source] | — |
|---|
| Unit cost | $1 million[source] | $1.25 million[source] |
|---|
| Produced | 1962[source] | 1987–present[source] |
|---|
| Warhead | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] | national ver. 300 kg semi-armour piercing HE, thermonuclear ; for export 200 kg semi-armour piercing HE[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | Ramjet 4 tons of thrust[source] |
|---|
| Propellant | Tonka-250 and IRFNA[source] | jet fuel[source] |
|---|
| Flight ceiling | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] | 14,000 m (46000 ft)[source] |
|---|
| Guidance system | Inertial guidance followed by terminal active radar homing[source] | midcourse inertial guidance , active radar homing - passive radar seeker head[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | 1.5 m[source] |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | coastal installations, naval ships , Fixed-wing aircraft[source] |
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| Manufacturer | MKB Raduga[source] | NPO Mashinostroyeniya[source] |
|---|
| Detonation mechanism | — | delay fuze[source] |
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| Flight altitude | — | 10 meters (32 ft) or higher[source] |
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| Reported operators |
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