Credit
Антон Бородин · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
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At a glance
Kh-22larger figure on 2 of 2
Ra'ad-II
Measured figures
Length
Single source11.65 m (38.2 ft)[source]
Length
Single sourceConfiguration
| Specification | Kh-22 | Ra'ad-II |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | ALCM[source] |
| Place of origin | Soviet Union[source] | Pakistan[source] |
| In service | 1968-present[source] | 2020 –Present[source] |
| Used by | Russia[source] | Pakistan Air Force Air Force Strategic Command[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
4.85 m (15.9 ft)[source]
Warhead weight
Single source450 kg (990 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] | National Engineering & Scientific Commission (Guidance/controls) Air Weapons Complex (Warhead design/assembly)[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] | ICM / HE / NE[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | Turbojet[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 , Terminal[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | 3.0 m (9.8 ft) CEP[source] |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | JF-17A/B , Mirage-IIIR , Mirage-VR[source] |
|---|
| Manufacturer | MKB Raduga[source] | Air Weapons Complex[source] |
|---|
| Designed | — | 2007–2019[source] |
|---|
| Developed into | — | Taimoor[source] |
|---|
| Blast yield | — | 5 kilotons of TNT (21 TJ)—12 kilotons of TNT (50 TJ)[source] |
|---|
| Payload capacity | — | ≤450 kg (990 lb)[source] |
|---|
| Flight altitude | — | Terrain-following[source] |
|---|
| Transport | — | Combat aircraft[source] |
|---|
| Role | — | standoff and an air-launched cruise missile (ALCM)[source] |
|---|
| Reported operators |
| — |
|---|