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At a glance
AGM-158 JASSMlarger figure on 0 of 3
Kh-22larger figure on 3 of 3
Measured figures
Length
Single source14 ft 1 in (4.287 m)[source]
Length
Single sourceConfiguration
| Specification | AGM-158 JASSM | Kh-22 |
|---|---|---|
| Type | Air-launched cruise missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | United States[source] | Soviet Union[source] |
| In service | 2003–present[source] | 1968-present[source] |
| Used by | United States Air Force Royal Australian Air Force Polish Air Force Finnish Air Force[source] | Russia |
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]
Maximum; Mach 4.6 (
Single sourceMaximum; Maximum speed
Single sourceMach 4.6 (5,600 km/h; 3,500 mph)[source]
Teledyne CAE J402-CA-100 turbojet
Single sourceTeledyne CAE J402-CA-100 turbojet 674 lbf (3 kN)[source]
Warhead weight
Single source1,000 lb (450 kg)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Syrian Civil War U.S. intervention in Syria Yemeni Civil War Operation Rough Rider 2026 Iran war[source] | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Designer | Lockheed Martin[source] | MKB Raduga[source] |
|---|
| Designed | 1995–1998[source] | — |
|---|
| Manufacturer | Lockheed Martin Missiles and Fire Control[source] | MKB Raduga[source] |
|---|
| Unit cost | $698,000 (JASSM Baseline AGM-158A, FY17)[source] | $1 million[source] |
|---|
| Produced | 1998–present[source] | 1962[source] |
|---|
| No. built | 7,500[source] | — |
|---|
| Warhead | WDU-42/B penetrator[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Detonation mechanism | FMU-156/B[source] | — |
|---|
| Guidance system | GPS , INS , IIR[source] | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Steering system | Moving wings & 2 tailplanes[source] | — |
|---|
| Accuracy | 9 ft 10 in (3 m) CEP[source] | >300 ft (91 m) (CEP)[source] |
|---|
| Launch platform | B-1 Lancer , B-2 Spirit , B-52 Stratofortress , F-15E Strike Eagle , F-16 Fighting Falcon , F/A-18 Hornet Rapid Dragon : C-130 , C-17[source] | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| References | Janes[source] | — |
|---|
| Engine | — | R-201 liquid-fuel rocket[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 | — |
|
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