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BCruise & anti-ship missiles
Cruise missile Land-attack missile Air-launched cruise missile Anti-ship missile Submarine-launched cruise missile
Measured figures
Maximum; 0.7 Mach. (subsonic)
Single source0.7 Mach. (subsonic) 990 km/h (620 mph)[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; >
Single source>1,500–2,000 km (930–1,240 mi; 810–1,080 nmi)[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.
Configuration
| Specification | Babur (cruise missile) | CJ-10 (missile) |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Cruise missile Land-attack missile Air-launched cruise missile Anti-ship missile Submarine-launched cruise missile[source] |
| In service | 2010 –Present[source] | — |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | China[source] |
| Designer | National Defence Complex[source] | — |
| Designed | 1998–2008 (GLCM) 2001–2018 (SLCM)[source] | — |
| Manufacturer | National Defence Complex[source] | China Aerospace Science and Industry Corporation /China Haiying Electro-Mechanical Technology Academy[source] |
| Developed from | BGM-109 Tomahawk[source] | — |
| Variants | See variants[source] | — |
| Warhead | HE / NE[source] | 500 kg (1,100 lb), conventional or nuclear[source] |
| Blast yield | 5 kilotons of TNT (21 TJ) – 12 kilotons of TNT (50 TJ)[source] | — |
| Engine | Turbojet[source] | — |
| Transmission | Automatic[source] | — |
| Suspension | WS2500 10WD[source] | — |
| Propellant | Liquid-propellant (jet engine) Solid-propellant (booster)[source] | — |
| Flight altitude | Terrain-following[source] | — |
| Guidance system | INS , TERCOM / DSMAC , GPS , GLONASS , Terminal ,[source] | INS / Sat / TERCOM DSMAC (terminal)[source] |
| Accuracy | 20 m (66 ft) CEP[source] | — |
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | Aircraft Transporter erector launcher Submarine Surface ship[source] |
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
| Country of origin | Pakistan[source] | — |
| Place of origin | — | China[source] |
| Alternative designation | — | CJ-10[source] |
| Reported operators | — |
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