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 | Otomat |
|---|---|---|
| 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 and land-attack missile[source] |
| Place of origin | India Russia[source] | Italy/France[source] |
| In service | 21 June 2007 – present[source] | 1977[source] |
| Used by | Indian Army Indian Navy Indian Air Force Philippine Marine Corps[source] | Italian Navy |
BrahMos: 8.4 m (28 ft) BrahMos-NG: 6 m (20 ft)[source]
Length
Single source6 m (19.7 ft)[source]
Maximum; 1.0 km/s
Single sourceMaximum; Mach 3 (
Single sourceMach 3 (3,700 km/h; 2,300 mph; 1.0 km/s)[source]
Maximum; Mach 0.91
Single sourceMaximum; Maximum speed · source measurement 1
Single sourceOperational; 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; MK2/E +
Single sourceOperational; Otomat Mk 2 Block IV TESEO
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| Wars | 2025 India–Pakistan conflict[source] | — |
|---|
| Designer | Defence Research and Development Organisation NPO Mashinostroyeniya[source] | — |
|---|
| Manufacturer | BrahMos Aerospace Limited[source] | MBDA[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] | 210 kg (463 lb)[source] |
|---|
| Engine | 1st Stage: Solid rocket booster [EEL] 2nd Stage: Liquid rocket ramjet [NPO][source] | Turbojet engine[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] | Inertial guidance , GPS and active radar homing[source] |
|---|
| Accuracy | 1 m CEP[source] | — |
|---|
| Launch platform | Warship Land-based TEL Submarine Fighter aircraft[source] | Surface-launched[source] |
|---|
| Detonation mechanism | — | Impact and proximity[source] |
|---|
| Reported operators |
| — |
|---|
Maximum; Maximum speed · source measurement 2
Single source310 m/s (690 mph; 1,100 km/h; Mach 0.91)[source]
Otomat Mk 2 Block IV: 180 km (97 nmi) TESEO MK2/E: 350 km (190 nmi)+[source]