FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
Measured figures
Configuration
| Specification | Babur (cruise missile) | Hwasal-1 |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Land-attack cruise missile[source] |
| In service | 2010 –Present[source] | 2021–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | Korean People's Army Strategic Force[source] |
| Designer | National Defence Complex[source] | — |
Wingspan
Single source2.50 m (8.2 ft)[source]
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; Operational range
Single source1,500–2,000 km (930–1,240 mi)[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] | North Korea[source] |
|---|
| Developed from | BGM-109 Tomahawk[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | HE / NE[source] | Conventional or tactical nuclear warhead[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 combined with TERCOM[source] |
|---|
| Accuracy | 20 m (66 ft) CEP[source] | — |
|---|
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | Transporter erector launcher[source] |
|---|
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
|---|
| Country of origin | Pakistan[source] | — |
|---|
| Place of origin | — | North Korea[source] |
|---|