Credit
Vitaly V. Kuzmin · CC BY-SA 4.0 · Resized · CC BY-SA 4.0 · Source ↗ · Modified
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At a glance
Buk missile systemlarger figure on 0 of 1
MT-12larger figure on 1 of 1
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Length
Single source5,550 millimetres (18 ft 3 in)[source]
Length
Single sourceConfiguration
| Specification | Buk missile system | MT-12 |
|---|---|---|
| Speed | Mach 3[source] | — |
| Type | Medium range SAM system[source] | Anti-tank gun[source] |
| Place of origin | Soviet Union; later Russia[source] | Soviet Union[source] |
| In service | 1980–present[source] | 1970–present[source] |
| Used by | 9K37 Buk § Operators |
9.65 m (31 ft 8 in)[source]
Diameter
Single sourcewingspan
Single source400 mm ( 15 + 3 ⁄ 4 in); wingspan 860 mm (2 ft 10 in)[source]
Warhead weight
Single source70 kg (150 lb)[source]
63 calibers
Single source6.3 m (20 ft 8 in) 63 calibers[source]
Rate of fire
Single source6-14 rpm[source]
Muzzle velocity
Single source700–1,575 m/s (2,300–5,170 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
See Operators[source] |
| Wars | Russo-Georgian War Russo-Ukrainian War War in Donbas Russo-Ukrainian war (2022–present) Second Nagorno-Karabakh War 2026 United States intervention in Venezuela[source] | See Wars[source] |
|---|
| Designer | Almaz-Antey : Tikhomirov NIIP (lead designer) Lyulev Novator (SA missile designer) MNIIRE Altair (naval version designer) NIIIP (surveillance radar designer) DNPP (missiles) UMZ (TELARs) MZiK (TELs) Kalashnikov : MMZ ( GM chassis )[source] | — |
|---|
| Designed | 1972[source] | — |
|---|
| Variants | Land: 9K37 "Buk" 9K37M 9K37M1 "Buk-M1" 9K37M1-2 "Buk-M1-2" 9K37M1-2A 9K317 "Buk-M2" 9K317M "Buk-M3" Naval: 3S90 (M-22) 3S90M 3S90E.1[source] | — |
|---|
| Warhead | Frag-HE[source] | — |
|---|
| Detonation mechanism | Radar proximity fuse[source] | — |
|---|
| Propellant | Solid propellant rocket[source] | — |
|---|
| Flight altitude | 14,000 metres (46,000 ft)[source] | — |
|---|
| Guidance system | Semi-active radar homing[source] | — |
|---|
| Launch platform | § System composition[source] | — |
|---|
| Shell | — | 100 × 910 mmR[source] |
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| Recoil | — | Hydro-pneumatic[source] |
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| Carriage | — | Transport: MT-LB On road: 70 km/h (43 mph) Off road: 25 km/h (16 mph)[source] |
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| Elevation | — | −6° to +20°[source] |
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| Traverse | — | 27° left or right[source] |
|---|
| Manufacturer | — | Yurga Machine-Building Plant[source] |
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| Reported operators |
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