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At a glance
Babur (cruise missile)larger figure on 0 of 4
Kh-22larger figure on 4 of 4
Measured figures
Length
Single source6.2 m (20 ft)[source]
Length
Single sourceConfiguration
| Specification | Babur (cruise missile) | Kh-22 |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| In service | 2010 –Present[source] | 1968-present[source] |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | Russia[source] |
| Designer | National Defence Complex[source] | MKB Raduga |
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; Maximum firing range
Single sourceOperational; Babur-I
Single sourceOperational; Babur-IA
Single sourceOperational; Babur-IB
Single sourceOperational; Babur-II
Single sourceOperational; Babur-III
Single sourceOperational; Harbah
Single sourceOperational; Harbah export variant
Single source900 km (560 mi)[source]
Babur-I: 700 km (430 mi) Babur-IA: 450 km Babur-II: 750 km (470 mi) Babur-III: 450 km (280 mi; 240 nmi) Harbah: 700 km (430 mi; 380 nmi) Babur-IB: 900 km (560 mi) Harbah export variant: 290 km (180 mi; 160 nmi)[source]
Operational; Kh-22M/MA
Single source600 km (320 nmi) (Kh-22M/MA)[source]
Warhead weight
Single source450 kg (990 lb) – 500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Designed | 1998–2008 (GLCM) 2001–2018 (SLCM)[source] | — |
|---|
| Manufacturer | National Defence Complex[source] | MKB Raduga[source] |
|---|
| Developed from | BGM-109 Tomahawk[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | HE / NE[source] | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Blast yield | 5 kilotons of TNT (21 TJ) – 12 kilotons of TNT (50 TJ)[source] | — |
|---|
| Engine | Turbojet[source] | R-201 liquid-fuel rocket[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | WS2500 10WD[source] | — |
|---|
| Propellant | Liquid-propellant (jet engine) Solid-propellant (booster)[source] | Tonka-250 and IRFNA[source] |
|---|
| Flight altitude | Terrain-following[source] | — |
|---|
| Guidance system | INS , TERCOM / DSMAC , GPS , GLONASS , Terminal ,[source] | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Accuracy | 20 m (66 ft) CEP[source] | >300 ft (91 m) (CEP)[source] |
|---|
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
|---|
| Country of origin | Pakistan[source] | — |
|---|
| Place of origin | — | Soviet Union[source] |
|---|
| Wars | — | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Unit cost | — | $1 million[source] |
|---|
| Produced | — | 1962[source] |
|---|
| Flight ceiling | — | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
|---|
| Reported operators | — |
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