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At a glance
Kalibr (missile family)larger figure on 0 of 1
Measured figures
Varies on variant, from
Single sourceVaries on variant, from 6.2 m to 8.9 m[source]
Length
Single sourceConfiguration
| Specification | Kalibr (missile family) | Kh-22 |
|---|---|---|
| Type | Cruise missile Anti-ship missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | Russia[source] | Soviet Union[source] |
| In service | 1994[source] | 1968-present[source] |
| Used by | See Operators[source] | Russia |
Kh-22larger figure on 1 of 1
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; 3M14K/3M14T domestic land-attack version, estimate
Single sourceOperational; 3M54E (export anti-ship version)
Single sourceOperational; 3M54E (export anti-ship version) 3M54E1/3M14E (export anti-ship version)
Single sourceOperational; 3M54K/3M54T domestic anti-ship version, estimate
Single source3M54E (export anti-ship version): 220 km 3M54E1/3M14E (export anti-ship version): 300 km 3M54K/3M54T: 660 km (domestic anti-ship version, estimate) 3M14K/3M14T: 1,500–2,500 km (domestic land-attack version, estimate)[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.
| Wars | Syrian Civil War Russo-Ukrainian War[source] | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Manufacturer | Novator Design Bureau , KTRV , MKB Fakel, NPO Mash, Raduga, NPO Zvezda Strela (Orenburg)[source] | MKB Raduga[source] |
|---|
| Unit cost | $980,000 (domestic cost, land-attack version) $6.5 million (export cost, anti-ship version)[source] | $1 million[source] |
|---|
| Produced | 1994–present[source] | 1962[source] |
|---|
| Warhead | 400–500 kg[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Engine | Multi-stage solid-fuel rocket, turbojet engine for 3M-54/E/TE/E1/TE1, -14/E/TE[source] | R-201 liquid-fuel rocket[source] |
|---|
| Flight ceiling | 1,000 m[source] | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
|---|
| Flight altitude | 50–150 m AGL 20 m over water[source] | — |
|---|
| Guidance system | Inertial guidance plus terminal active radar homing[source] | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Accuracy | 2–3 m (domestic version, with GLONASS ) 50 m CEP (Club-T export version, without GLONASS )[source] | >300 ft (91 m) (CEP)[source] |
|---|
| Launch platform | naval ships , submarines , containers , TEL[source] | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| Designer | — | MKB Raduga[source] |
|---|
| Propellant | — | Tonka-250 and IRFNA[source] |
|---|
| Reported operators |
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