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At a glance
Babur (cruise missile)larger figure on 4 of 4
R-360 Neptunelarger figure on 0 of 4
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
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; for Long Neptune
Single sourceOperational; Over up to
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | Babur (cruise missile) | R-360 Neptune |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Anti-ship missile Cruise missile[source] |
| In service | 2010 –Present[source] | 2021–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | Ukrainian Navy[source] |
| Designer | National Defence Complex[source] | Luch Design Bureau[source] |
| Designed | 1998–2008 (GLCM) 2001–2018 (SLCM)[source] | — |
| Manufacturer | National Defence Complex[source] | KhAZ[source] |
| Developed from | BGM-109 Tomahawk[source] | — |
| Variants | See variants[source] | — |
| Warhead | HE / NE[source] | — |
| Blast yield | 5 kilotons of TNT (21 TJ) – 12 kilotons of TNT (50 TJ)[source] | — |
| Engine | Turbojet[source] | Motor Sich MS400 turbofan[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] | — |
| Accuracy | 20 m (66 ft) CEP[source] | — |
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | — |
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
| Country of origin | Pakistan[source] | — |
| Place of origin | — | Ukraine[source] |
| Wars | — | Russo-Ukrainian War[source] |
Over 280 km (170 mi) up to 1,000 km (620 mi) for Long Neptune[source]