Credit
Антон Бородин · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
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BCruise & anti-ship missiles
Air-to-surface Surface-to-surface missile Cruise missile Anti-ship missile Land-attack missile
At a glance
Kh-22larger figure on 3 of 3
Measured figures
Length
Single source11.65 m (38.2 ft)[source]
air version
Single sourceConfiguration
| Specification | Kh-22 | Kh-35 |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Air-to-surface Surface-to-surface missile Cruise missile Anti-ship missile Land-attack missile[source] |
| Place of origin | Soviet Union[source] | Soviet Union[source] |
| In service | 1968-present[source] | 2003[source] |
| Used by | Russia[source] | Russian Navy Indian Navy Vietnam People's Navy[source] |
Kh-35larger figure on 0 of 3
Counts only measures both sources give with the same scope. A larger figure is not a better system.
surface & heli version
Single source385 cm (152 in) (air version) 440 cm (173 in) (surface & heli version)[source]
Maximum; Maximum speed
Single sourceMaximum; Mach 4.6 (
Single sourceMach 4.6 (5,600 km/h; 3,500 mph)[source]
Maximum; Maximum speed
Single sourceMaximum; Mach 0.8 – Mach 0.85 (
Single sourceWarhead weight
Single source145 kg (320 lb)[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] | Zvezda[source] |
|---|
| Unit cost | $1 million[source] | $500,000 (2010)[source] |
|---|
| Produced | 1962[source] | 1996 for export, 2003 for Russia[source] |
|---|
| Warhead | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] | HE fragmentation shaped charge[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | R95TP-300 Turbofan 360 kgf[source] |
|---|
| Propellant | Tonka-250 and IRFNA[source] | kerosene[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 guidance and ARGS-35E X-band terminal active radar homing[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | — |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | Tupolev Tu-142 , Su-24 , MiG-29 M/K, Sukhoi Su-35 , Su-27 SM, Su-30MKI // Su-30SM , Su-34 , HAL Tejas , Ka-27 , Ka-28 , Ka-52 , Su-57 , also ships and boats, coastal, ALCM , TEL variants.[source] |
|---|
| Manufacturer | MKB Raduga[source] | Tactical Missiles Corporation[source] |
|---|
| Designed | — | 1983–2003[source] |
|---|
| Flight altitude | — | 10-15 m en route and about 4 m at terminal area[source] |
|---|
| Reported operators |
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|---|
Mach 0.8 – Mach 0.85 (609–647 mph; 980–1,041 km/h)[source]