FORCETALLY
Loading the evidence…
Preparing your view.
Preparing your view.
At a glance
Babur (cruise missile)larger figure on 2 of 2
Otomatlarger figure on 0 of 2
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source6.2 m (20 ft)[source]
Length
Single sourceConfiguration
| Specification | Babur (cruise missile) | Otomat |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Anti-ship missile and land-attack missile[source] |
| In service | 2010 –Present[source] | 1977[source] |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | Italian Navy[source] |
| Designer | National Defence Complex[source] | — |
6 m (19.7 ft)[source]
Maximum; 0.7 Mach. (subsonic)
Single source0.7 Mach. (subsonic) 990 km/h (620 mph)[source]
Maximum; Mach 0.91
Single sourceMaximum; Maximum speed · source measurement 1
Single sourceMaximum; Maximum speed · source measurement 2
Single source310 m/s (690 mph; 1,100 km/h; Mach 0.91)[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; MK2/E +
Single sourceOperational; Otomat Mk 2 Block IV TESEO
Single sourceWarhead 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] | MBDA[source] |
|---|
| Developed from | BGM-109 Tomahawk[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | HE / NE[source] | 210 kg (463 lb)[source] |
|---|
| Blast yield | 5 kilotons of TNT (21 TJ) – 12 kilotons of TNT (50 TJ)[source] | — |
|---|
| Engine | Turbojet[source] | Turbojet engine[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] | Inertial guidance , GPS and active radar homing[source] |
|---|
| Accuracy | 20 m (66 ft) CEP[source] | — |
|---|
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | Surface-launched[source] |
|---|
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
|---|
| Country of origin | Pakistan[source] | — |
|---|
| Place of origin | — | Italy/France[source] |
|---|
| Detonation mechanism | — | Impact and proximity[source] |
|---|
Otomat Mk 2 Block IV: 180 km (97 nmi) TESEO MK2/E: 350 km (190 nmi)+[source]