Preparing your view.
ACruise & anti-ship missiles
Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile
At a glance
Measured figures
BrahMos
Single sourceBrahMos-NG
Single sourceConfiguration
| Specification | BrahMos | R-360 Neptune |
|---|---|---|
| Type | Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile[source] | Anti-ship missile Cruise missile[source] |
| Place of origin | India Russia[source] | Ukraine[source] |
| In service | 21 June 2007 – present[source] | 2021–present[source] |
| Used by | Indian Army Indian Navy Indian Air Force Philippine Marine Corps[source] | Ukrainian Navy |
BrahMos: 8.4 m (28 ft) BrahMos-NG: 6 m (20 ft)[source]
Length
Single source5.05 m (16.6 ft)[source]
Operational; Air platform
Single sourceOperational; Export
Single sourceOperational; Ship or Land platform
Single sourceShip or Land platform : 800–900 km (500–560 mi) Air platform : 450–500 km (280–310 mi) Export : 290 km (180 mi)[source]
Operational; for Long Neptune
Single sourceOperational; Over up to
Single sourceNeptune Long Neptune
Single sourceWarhead weight
Single sourceNeptune 150 kg (330 lb) Long Neptune 260 kg (570 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | 2025 India–Pakistan conflict[source] | Russo-Ukrainian War[source] |
|---|
| Designer | Defence Research and Development Organisation NPO Mashinostroyeniya[source] | Luch Design Bureau[source] |
|---|
| Manufacturer | BrahMos Aerospace Limited[source] | KhAZ[source] |
|---|
| Unit cost | BrahMos: US$ 3.5 million BrahMos-ER: US$ 4.85 million[source] | — |
|---|
| Variants | Ship-launched Land-launched Submarine-launched Air-launched BrahMos-ER BrahMos-NG BrahMos-II[source] | — |
|---|
| Warhead | 200–300 kg (440–660 lb) nuclear conventional semi- armour-piercing warhead[source] | — |
|---|
| Engine | 1st Stage: Solid rocket booster [EEL] 2nd Stage: Liquid rocket ramjet [NPO][source] | Motor Sich MS400 turbofan[source] |
|---|
| Propellant | 1st Stage: Solid fuel 2nd Stage: Liquid fuel[source] | — |
|---|
| Flight ceiling | 15 km (49,000 ft)[source] | — |
|---|
| Flight altitude | Sea skimming , as low as 3 to 10 meters[source] | — |
|---|
| Guidance system | Mid-course: INS + multi- GNSS Terminal: ARH[source] | — |
|---|
| Accuracy | 1 m CEP[source] | — |
|---|
| Launch platform | Warship Land-based TEL Submarine Fighter aircraft[source] | — |
|---|
| Reported operators |
| — |
|---|
Over 280 km (170 mi) up to 1,000 km (620 mi) for Long Neptune[source]