ACruise & anti-ship missiles
Joint Strike Missile
Air-launched anti-ship and land-attack cruise missile
Preparing your view.
ACruise & anti-ship missiles
Air-launched anti-ship and land-attack cruise missile


At a glance
Joint Strike Missilelarger figure on 0 of 2
Kh-22larger figure on 2 of 2
Measured figures
Length
Single source4.00 m (13 ft 1 in)[source]
Length
Single sourceConfiguration
| Specification | Joint Strike Missile | Kh-22 |
|---|---|---|
| Type | Air-launched anti-ship and land-attack cruise missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | Norway United States[source] | Soviet Union[source] |
| Designer | Kongsberg Defence & Aerospace Raytheon Missiles & Defense[source] | MKB Raduga[source] |
| Designed | From 2008 until mid-2018[source] | — |
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]
stowed
Single source480 mm (1 ft 7 in) stowed[source]
Maximum; ) estimated
Single sourceMaximum; Mach 0.9 (
Single sourceMach 0.9 (310 m/s; 1,000 ft/s) estimated[source]
Maximum; Mach 4.6 (
Single sourceMaximum; Maximum speed
Single sourceOperational; hi‐hi‐lo >
Single sourceOperational; lo‐lo‐lo
Single sourceOperational; Operational range
Single source555 km (345 mi; 300 nmi) hi‐hi‐lo >350 km (220 mi; 190 nmi) 185 km (115 mi; 100 nmi) lo‐lo‐lo[source]
Operational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Warhead weight
Single source120 kg (260 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Manufacturer | Kongsberg Defence & Aerospace Raytheon Missiles & Defense[source] | MKB Raduga[source] |
|---|
| Developed from | Naval Strike Missile[source] | — |
|---|
| Produced | 2021[source] | 1962[source] |
|---|
| Warhead | Blast-fragmentation[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Detonation mechanism | Time delay, impact[source] | — |
|---|
| Blast yield | 100 kg (220 lb) TNT equivalent[source] | — |
|---|
| Engine | Williams International F‐415 small turbofan[source] | R-201 liquid-fuel rocket[source] |
|---|
| Guidance system | GPS , INS , TERCOM , Imaging Infrared (IIR) capable of Autonomous Target Recognition (ATR), Passive RF homing capabilities for attacking radar-emitting threats, Two-way datalink[source] | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Accuracy | CEP 1 m (3 ft 3 in)[source] | >300 ft (91 m) (CEP)[source] |
|---|
| Launch platform | Fighters: F-15E , F-16 , F/A-18E/F , F-35A and F-35C (internally) Planned: Fighters: Eurofighter Typhoon Drones: GA-ASI MQ-9B SkyGuardian Submarines: Type 212CD class , S-80 Plus class , Orka class[source] | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| References | Janes[source] | — |
|---|
| In service | — | 1968-present[source] |
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| Used by | — | Russia[source] |
|---|
| Wars | — | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Unit cost | — | $1 million[source] |
|---|
| Propellant | — | Tonka-250 and IRFNA[source] |
|---|
| Flight ceiling | — | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
|---|
| Reported operators | — |
|
|---|
Mach 4.6 (5,600 km/h; 3,500 mph)[source]