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BCruise & anti-ship missiles
Cruise missile Air-launched cruise missile Air-to-surface missile Anti-ship missile Land-attack missile
At a glance
Kh-22larger figure on 5 of 5
Measured figures
Length
Single source11.65 m (38.2 ft)[source]
Length
Single sourceConfiguration
| Specification | Kh-22 | Kh-59 |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Cruise missile Air-launched cruise missile Air-to-surface missile Anti-ship missile Land-attack missile[source] |
| Place of origin | Soviet Union[source] | Soviet Union / Russia[source] |
| In service | 1968-present[source] | 1980–current[source] |
| Used by | Russia[source] |
Kh-59larger figure on 0 of 5
Counts only measures both sources give with the same scope. A larger figure is not a better system.
570 cm (220 in)[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 0.72 – Mach 0.88 (
Single sourceOperational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Operational; Kh-59ME
Single sourceOperational; Kh-59ME (export)
Single sourceOperational; Kh-59MK
Single sourceOperational; Kh-59MK2
Single sourceKh-59ME (export): 115 km (62 nmi) Kh-59ME: 200 km (110 nmi) Kh-59MK: 285 km (150 nmi) Kh-59MK2: 290 km (160 nmi)[source]
Warhead weight
Single source320 kg (705 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Russia, China, India, Algeria[source] |
| Wars | Russo-Ukrainian War Russo-Ukrainian war[source] | First Chechen War Second Chechen War Russo-Ukrainian War[source] |
|---|
| Designer | MKB Raduga[source] | 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] | Cluster or shaped-charge fragmentation[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | Kh-59: two-stage rocket Kh-59ME: rocket then R95TP-300 turbojet/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] | Inertial guidance (then TV guidance ), millimeter wave active radar homing (Kh-59MK, Kh-59MK2 land attack version)[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | — |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | Kh-59ME: Su-30MK Kh-59: Su-24M, MiG-27, Su-17M3/22M4, HAL Tejas , Su-30 MKI Su-25 and Su-30 Kh-59MK2: Su-57[source] |
|---|
| Manufacturer | MKB Raduga[source] | Tactical Missiles Corporation[source] |
|---|
| Reported operators |
| — |
|---|
Mach 0.72 – Mach 0.88 (882–1,080 km/h; 548–670 mph)[source]