FORCETALLY
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Measured figures
Configuration
| Specification | Abu Mahdi (missile) | Kh-22 |
|---|---|---|
| Type | Cruise missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | Iran[source] | Soviet Union[source] |
| In service | 20 August 2020[source] | 1968-present[source] |
| Used by | Iran[source] | Russia |
Wingspan
Single source300 cm (120 in)[source]
Maximum; Mach 4.6 (
Single sourceMaximum; Maximum speed
Single sourceMach 4.6 (5,600 km/h; 3,500 mph)[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.
| Warhead | High Explosive[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Wars | — | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Designer | — | MKB Raduga[source] |
|---|
| Unit cost | — | $1 million[source] |
|---|
| Produced | — | 1962[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] |
|---|
| Guidance system | — | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Accuracy | — | >300 ft (91 m) (CEP)[source] |
|---|
| Launch platform | — | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| Manufacturer | — | MKB Raduga[source] |
|---|
| Reported operators | — |
|
|---|