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BCruise & anti-ship missiles
Cruise missile Air-launched cruise missile Submarine-launched cruise missile Anti-ship missile Surface-to-surface missile Land-attack missile
At a glance
Babur (cruise missile)larger figure on 1 of 4
P-800 Onikslarger figure on 3 of 4
Measured figures
Length
Single source6.2 m (20 ft)[source]
Length
Single sourceConfiguration
| Specification | Babur (cruise missile) | P-800 Oniks |
|---|---|---|
| Type | GLCM / SLCM / AshM[source] | Cruise missile Air-launched cruise missile Submarine-launched cruise missile Anti-ship missile Surface-to-surface missile Land-attack missile[source] |
| In service | 2010 –Present[source] | 2002–present[source] |
| Used by | Pakistan Army ( Army Strategic Forces ) Pakistan Navy ( Navy Strategic Forces )[source] | See Operators[source] |
| Designer | National Defence Complex[source] |
Counts only measures both sources give with the same scope. A larger figure is not a better system.
8.9 m (29.2 ft)[source]
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; depending on altitude ( Yakhont export version)
Single sourceOperational; Oniks-M version for Russia
Single sourceWarhead weight
Single source450 kg (990 lb) – 500 kg (1,100 lb)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
| — |
| Designed | 1998–2008 (GLCM) 2001–2018 (SLCM)[source] | — |
|---|
| Manufacturer | National Defence Complex[source] | NPO Mashinostroyeniya[source] |
|---|
| Developed from | BGM-109 Tomahawk[source] | — |
|---|
| Variants | See variants[source] | — |
|---|
| Warhead | HE / NE[source] | national ver. 300 kg semi-armour piercing HE, thermonuclear ; for export 200 kg semi-armour piercing HE[source] |
|---|
| Blast yield | 5 kilotons of TNT (21 TJ) – 12 kilotons of TNT (50 TJ)[source] | — |
|---|
| Engine | Turbojet[source] | Ramjet 4 tons of thrust[source] |
|---|
| Transmission | Automatic[source] | — |
|---|
| Suspension | WS2500 10WD[source] | — |
|---|
| Propellant | Liquid-propellant (jet engine) Solid-propellant (booster)[source] | jet fuel[source] |
|---|
| Flight altitude | Terrain-following[source] | 10 meters (32 ft) or higher[source] |
|---|
| Guidance system | INS , TERCOM / DSMAC , GPS , GLONASS , Terminal ,[source] | midcourse inertial guidance , active radar homing - passive radar seeker head[source] |
|---|
| Accuracy | 20 m (66 ft) CEP[source] | 1.5 m[source] |
|---|
| Launch platform | Transporter erector launcher Cruise-missile submarine[source] | coastal installations, naval ships , Fixed-wing aircraft[source] |
|---|
| Transport | TEL , Horizontal launch tube (HLT)[source] | — |
|---|
| Country of origin | Pakistan[source] | — |
|---|
| Place of origin | — | Soviet Union / Russia[source] |
|---|
| Wars | — | Syrian Civil War Russo-Ukrainian war[source] |
|---|
| Unit cost | — | $1.25 million[source] |
|---|
| Produced | — | 1987–present[source] |
|---|
| Detonation mechanism | — | delay fuze[source] |
|---|
| Flight ceiling | — | 14,000 m (46000 ft)[source] |
|---|
| Reported operators | — |
|
|---|
Operational; Oniks version for Russia
Single source600 km (370 mi; 320 nmi) ( Oniks version for Russia) 800 km (500 mi; 430 nmi) ( Oniks-M version for Russia) 120 to 300 km (75 to 186 mi; 65 to 162 nmi) depending on altitude ( Yakhont export version)[source]