FORCETALLY
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BCruise & anti-ship missiles
Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile
Measured figures
BrahMos
Single sourceBrahMos-NG
Single sourceConfiguration
| Specification | Abu Mahdi (missile) | BrahMos |
|---|---|---|
| Type | Cruise missile[source] | Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile Submarine-launched cruise missile[source] |
| Place of origin | Iran[source] | India Russia[source] |
| In service | 20 August 2020[source] | 21 June 2007 – present[source] |
| Used by | Iran[source] |
BrahMos: 8.4 m (28 ft) BrahMos-NG: 6 m (20 ft)[source]
BrahMos
Single sourceBrahMos-NG
Single sourceBrahMos: 0.6 m (2.0 ft) BrahMos-NG: 0.5 m (1.6 ft)[source]
BrahMos
Single sourceBrahMos-A
Single sourceBrahMos-NG
Single sourceBrahMos: 3,000 kg (6,600 lb) BrahMos-A: 2,500 kg (5,500 lb) BrahMos-NG: 1,200–1,500 kg (2,600–3,300 lb)[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]
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]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Indian Army Indian Navy Indian Air Force Philippine Marine Corps[source] |
| Warhead | High Explosive[source] | 200–300 kg (440–660 lb) nuclear conventional semi- armour-piercing warhead[source] |
|---|
| Wars | — | 2025 India–Pakistan conflict[source] |
|---|
| Designer | — | Defence Research and Development Organisation NPO Mashinostroyeniya[source] |
|---|
| Manufacturer | — | BrahMos Aerospace Limited[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] |
|---|
| Engine | — | 1st Stage: Solid rocket booster [EEL] 2nd Stage: Liquid rocket ramjet [NPO][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 | — |
|
|---|