Loading the evidence…
Preparing your view.
Preparing your view.

At a glance
BM-14larger figure on 3 of 5
M270 Multiple Launch Rocket Systemlarger figure on 2 of 5
Counts only measures both sources give with the same scope. A larger figure is not a better system.
Measured figures
Muzzle velocity
Single source400 m/s (1,300 ft/s)[source]
Bars compare reported quantities only. A larger figure does not make a system better; configurations and test conditions differ.
Configuration
| Specification | BM-14 | M270 Multiple Launch Rocket System |
|---|---|---|
| Type | Multiple rocket launcher[source] | Multiple rocket launcher[source] |
| Place of origin | Soviet Union[source] | United States[source] |
| In service | 1952–present[source] | 1983–present[source] |
| Wars | Vietnam War Cambodian Civil War Cambodian–Vietnamese War Dhofar War Indonesian invasion of East Timor South African Border War Angolan Civil War Lebanese Civil War Soviet–Afghan War Algerian Civil War Somali Civil War War in Afghanistan (2001–2021) Syrian civil war[source] | Persian Gulf War War in Afghanistan Iraq War Russo-Ukrainian War Russian invasion of Ukraine Gaza war[source] |
| Designer | NII 303[source] | Ling-Temco-Vought[source] |
| Designed | 1950[source] | 1977[source] |
| Barrels | 16 in two rows[source] | — |
| Elevation | +50°/0°[source] | — |
| Traverse | 180°[source] | — |
| Suspension | Wheeled GAZ-63 4x4 chassis[source] | Torsion bar[source] |
| Used by | — | See Operators[source] |
| Manufacturer | — | Lockheed Martin Diehl BGT Defence Krauss-Maffei Wegmann Aérospatiale - Matra[source] |
| Unit cost | — | Domestic cost: $2.3 million per one launcher (FY 1990) $4.9 million (in 2024) per one launcher $168,000 per one M31 GMLRS (FY 2023) Export cost: $434,000 per one M31ER GMLRS (FY 2022)[source] |
| Produced | — | 1980–present[source] |
| Variants | — | M270, M270A1, M270A2, MARS II , LRU, MLRS-I[source] |
| Rate of fire | — | M26 : ~3s per round ATACMS : ~30s per round[source] |
| Armor | — | 5083 aluminum hull, 7039 aluminum cab[source] |
| Main armament | — | 12 × MLRS or 4 x PrSM or 2 × MGM-140 ATACMS[source] |
| Power/weight | — | 18.9 hp/ST (15.5 kW/t) (M270)[source] |
| Transmission | — | Cross-drive turbo transmission, fully electronically controlled[source] |
| Entered service | — | 1982, US Army[source] |
| First use in action | — | 1991, Gulf War[source] |
| Weight loaded | — | 54,578 pounds (24,756 kg)[source] |
| Height (stowed) | — | 8 ft 5 in (2.57 m)[source] |
| Height (max. elevation) | — | not available[source] |
| Maximum road speed | — | 40 mph (64 km/h)[source] |
| Cruise range | — | 300 miles (480 km)[source] |
| Reload time | — | 4 minutes (M270) 3 minutes (M270A1)[source] |
| Average unit cost | — | $2.3 million per launcher (FY 1990), $168,000 per M31 GMLRS rocket (FY 2023)[source] |
| Reported operators |
|
|
Effective; M26
Single sourceEffective; M26A1/A2
Single sourceEffective; M30/31
Single sourceMaximum; ATACMS : 103 or 165 or
Single source