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At a glance
Babur (cruise missile)larger figure on 0 of 1
Kalibr (missile family)larger figure on 1 of 1
Measured figures
Length
Single source6.2 m (20 ft)[source]
Varies on variant, from
Single sourceConfiguration
| Specification | Babur (cruise missile) | Kalibr (missile family) |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Cruise missile Anti-ship missile[source] |
| In service | 2010 –Present[source] | 1994[source] |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | See Operators[source] |
| Designer | National Defence Complex[source] | — |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Varies on variant, from 6.2 m to 8.9 m[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; 3M14K/3M14T domestic land-attack version, estimate
Single sourceOperational; 3M54E (export anti-ship version)
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] | Novator Design Bureau , KTRV , MKB Fakel, NPO Mash, Raduga, NPO Zvezda Strela (Orenburg)[source] |
|---|
| Developed from | BGM-109 Tomahawk[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | HE / NE[source] | 400–500 kg[source] |
|---|
| Blast yield | 5 kilotons of TNT (21 TJ) – 12 kilotons of TNT (50 TJ)[source] | — |
|---|
| Engine | Turbojet[source] | Multi-stage solid-fuel rocket, turbojet engine for 3M-54/E/TE/E1/TE1, -14/E/TE[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | WS2500 10WD[source] | — |
|---|
| Propellant | Liquid-propellant (jet engine) Solid-propellant (booster)[source] | — |
|---|
| Flight altitude | Terrain-following[source] | 50–150 m AGL 20 m over water[source] |
|---|
| Guidance system | INS , TERCOM / DSMAC , GPS , GLONASS , Terminal ,[source] | Inertial guidance plus terminal active radar homing[source] |
|---|
| Accuracy | 20 m (66 ft) CEP[source] | 2–3 m (domestic version, with GLONASS ) 50 m CEP (Club-T export version, without GLONASS )[source] |
|---|
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | naval ships , submarines , containers , TEL[source] |
|---|
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
|---|
| Country of origin | Pakistan[source] | — |
|---|
| Place of origin | — | Russia[source] |
|---|
| Wars | — | Syrian Civil War Russo-Ukrainian War[source] |
|---|
| Unit cost | — | $980,000 (domestic cost, land-attack version) $6.5 million (export cost, anti-ship version)[source] |
|---|
| Produced | — | 1994–present[source] |
|---|
| Flight ceiling | — | 1,000 m[source] |
|---|
| Reported operators | — |
|
|---|
Operational; 3M54E (export anti-ship version) 3M54E1/3M14E (export anti-ship version)
Single sourceOperational; 3M54K/3M54T domestic anti-ship version, estimate
Single source3M54E (export anti-ship version): 220 km 3M54E1/3M14E (export anti-ship version): 300 km 3M54K/3M54T: 660 km (domestic anti-ship version, estimate) 3M14K/3M14T: 1,500–2,500 km (domestic land-attack version, estimate)[source]