Credit
Антон Бородин · CC BY-SA 3.0 · Resized · CC BY-SA 3.0 · Source ↗ · Modified
FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Kh-22larger figure on 4 of 4
Measured figures
Length
Single source11.65 m (38.2 ft)[source]
Length
Single sourceConfiguration
| Specification | Kh-22 | NASM-MR |
|---|---|---|
| Type | Anti-ship cruise missile Air-to-surface missile[source] | Naval anti-ship missile[source] |
| Place of origin | Soviet Union[source] | India[source] |
| In service | 1968-present[source] | — |
| Used by | Russia[source] | Indian Navy (intended)[source] |
| Wars | Russo-Ukrainian War Russo-Ukrainian war |
NASM-MRlarger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
5.2 m (17 ft)[source]
Warhead weight
Single source150 kg (330 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designer | MKB Raduga[source] | Defence Research and Development Organisation[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] | PCB[source] |
|---|
| Engine | R-201 liquid-fuel rocket[source] | Solid booster + 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] | Mid-course: INS + GNSS + radar altimeter + two-way datalink Terminal: ARH[source] |
|---|
| Accuracy | >300 ft (91 m) (CEP)[source] | — |
|---|
| Launch platform | Tu-22M, Тu-22К, Тu-95К22[source] | HAL Tejas , Mikoyan MiG-29K , HAL TEDBF , Warships , Submarine , Tata LPTA 3138 HMV[source] |
|---|
| Manufacturer | MKB Raduga[source] | — |
|---|
| Reported operators |
| — |
|---|