ACruise & anti-ship missiles
BrahMos-II
Hypersonic Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile
FORCETALLY
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ACruise & anti-ship missiles
Hypersonic Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile
Measured figures
Configuration
| Specification | BrahMos-II | Kh-22 |
|---|---|---|
| Type | Hypersonic Cruise missile Air-launched cruise missile Anti-ship missile Land-attack missile Surface-to-surface missile[source] | Anti-ship cruise missile Air-to-surface missile[source] |
| Place of origin | India Russia[source] | Soviet Union[source] |
| Designer | Defence Research and Development Organisation NPO Mashinostroyenia[source] | MKB Raduga[source] |
| Manufacturer | BrahMos Aerospace Limited[source] |
Wingspan
Single source300 cm (120 in)[source]
Maximum; Mach 8 (
Single sourceMaximum; Maximum speed · source measurement 2
Single sourceMaximum; Maximum speed · source measurement 3
Single sourceMach 8 (9,800 km/h; 6,100 mph; 2,700 m/s)[source]
Maximum; Mach 4.6 (
Single sourceMaximum; Maximum speed
Single sourceBars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
MKB Raduga[source] |
| Unit cost | $12.5 million (est.)[source] | $1 million[source] |
|---|
| Engine | Scramjet[source] | R-201 liquid-fuel rocket[source] |
|---|
| Launch platform | Ship, submarine, aircraft and land-based mobile launchers.[source] | Tu-22M, Тu-22К, Тu-95К22[source] |
|---|
| In service | — | 1968-present[source] |
|---|
| Used by | — | Russia[source] |
|---|
| Wars | — | Russo-Ukrainian War Russo-Ukrainian war[source] |
|---|
| Produced | — | 1962[source] |
|---|
| Warhead | — | 1,000 kg (2,205 lb) RDX or 350–1,000 kt (1.5–4.2 PJ) thermonuclear weapon[source] |
|---|
| Propellant | — | Tonka-250 and IRFNA[source] |
|---|
| Flight ceiling | — | 10–14 km (33,000–46,000 ft) or 27 km (89,000 ft)[source] |
|---|
| Guidance system | — | Inertial guidance followed by terminal active radar homing[source] |
|---|
| Accuracy | — | >300 ft (91 m) (CEP)[source] |
|---|
| Reported operators | — |
|
|---|
Mach 4.6 (5,600 km/h; 3,500 mph)[source]