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At a glance
AGM-158 JASSMlarger figure on 1 of 4
Babur (cruise missile)larger figure on 3 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source14 ft 1 in (4.287 m)[source]
Length
Single sourceConfiguration
| Specification | AGM-158 JASSM | Babur (cruise missile) |
|---|---|---|
| Type | Air-launched cruise missile[source] | GLCM / SLCM / AshM[source] |
| Place of origin | United States[source] | — |
| In service | 2003–present[source] | 2010 –Present[source] |
| Used by | United States Air Force Royal Australian Air Force Polish Air Force Finnish Air Force[source] | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] |
6.2 m (20 ft)[source]
Maximum; 0.7 Mach. (subsonic)
Single source0.7 Mach. (subsonic) 990 km/h (620 mph)[source]
Operational; Operational range
Single source230 mi (370.4 km)[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]
Teledyne CAE J402-CA-100 turbojet
Single sourceTeledyne CAE J402-CA-100 turbojet 674 lbf (3 kN)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | Syrian Civil War U.S. intervention in Syria Yemeni Civil War Operation Rough Rider 2026 Iran war[source] | — |
|---|
| Designer | Lockheed Martin[source] | National Defence Complex[source] |
|---|
| Designed | 1995–1998[source] | 1998–2008 (GLCM) 2001–2018 (SLCM)[source] |
|---|
| Manufacturer | Lockheed Martin Missiles and Fire Control[source] | National Defence Complex[source] |
|---|
| Unit cost | $698,000 (JASSM Baseline AGM-158A, FY17)[source] | — |
|---|
| Produced | 1998–present[source] | — |
|---|
| No. built | 7,500[source] | — |
|---|
| Warhead | WDU-42/B penetrator[source] | HE / NE[source] |
|---|
| Detonation mechanism | FMU-156/B[source] | — |
|---|
| Guidance system | GPS , INS , IIR[source] | INS , TERCOM / DSMAC , GPS , GLONASS , Terminal ,[source] |
|---|
| Steering system | Moving wings & 2 tailplanes[source] | — |
|---|
| Accuracy | 9 ft 10 in (3 m) CEP[source] | 20 m (66 ft) CEP[source] |
|---|
| Launch platform | B-1 Lancer , B-2 Spirit , B-52 Stratofortress , F-15E Strike Eagle , F-16 Fighting Falcon , F/A-18 Hornet Rapid Dragon : C-130 , C-17[source] | Transporter erector launcher Cruise-missile submarine[source] |
|---|
| References | Janes[source] | — |
|---|
| Developed from | — | BGM-109 Tomahawk[source] |
|---|
| Variants | — | See variants[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] |
|---|
| Transport | — | TEL , Horizontal launch tube (HLT)[source] |
|---|
| Country of origin | — | Pakistan[source] |
|---|