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M270 American Multiple Launch Rocket System (MLRS)

M270

Multiple Launch Rocket System (MLRS)
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Basic Information
Name
M270 American Multiple Launch Rocket System (MLRS)
Designation
M270
Alternate Designation
M270
Equipment Type
Multiple Launch Rocket System (MLRS)
Manufacturer
Date of Introduction
1983
Description

The M270 Multiple Launch Rocket System (M270 MLRS) is an armored, self-propelled, multiple rocket launcher (a type of rocket artillery). Since the first M270s were delivered to the U.S. Army in 1983, the MLRS has been adopted by several NATO countries. Some 1,300 M270 systems have been manufactured in the United States and in Europe, along with more than 700,000 rockets. The production of the M270 ended in 2003, when a last batch was delivered to the Egyptian Army. MLRS was developed jointly by the United Kingdom, United States, West Germany, France and Italy, developed from the older General Support Rocket System (GSRS). The M270 MLRS weapons system is collectively known as the M270 MLRS Self-Propelled Loader/Launcher (SPLL). The SPLL is composed of three primary subsystems: the M269 Loader Launcher Module (LLM), which also houses the electronic Fire Control System, is mated to the M993 Carrier Vehicle. The M993 is a derivative of the Bradley Fighting Vehicle chassis. Cold War doctrine for the M270 was for the vehicles to spread out individually and hide until needed, then move to a firing position and launch their rockets, immediately move away to a reloading point, then move to a completely new hiding position near a different firing point. These shoot-and-scoot tactics were planned to avoid susceptibility to Soviet counterbattery fire. One M270 firing 12 M26 rockets would drop 7,728 bomblets, and one MLRS battery firing 108 rockets had the equivalent firepower of 33 battalions of cannon artillery. The system can fire rockets or MGM-140 ATACMS missiles, which are contained in interchangeable pods. Each pod contains six standard rockets or one guided ATACMS missile; the two types cannot be mixed. The LLM can hold two pods at a time, which are hand-loaded using an integrated winch system. All twelve rockets or two ATACMS missiles can be fired in under a minute. One launcher firing twelve rockets can completely blanket one square kilometer with submunitions. For this reason, the MLRS is sometimes referred to as the "Grid Square Removal System" (metric maps are usually divided up into 1 km grids). Or informally among artillery personnel as "the finger of God", since a single launcher can sanitize an entire grid square, which is about the size of a fingertip on a typical map. A typical MLRS cluster salvo consisted of three M270 vehicles each firing all 12 rockets. With each rocket containing 644 M77 grenades, the entire salvo would drop 23,184 grenades in the target area. However, with a two percent dud rate, that would leave approximately 400 undetonated bombs scattered over the area, which could endanger friendly troops and civilians. In 2006, MLRS was upgraded to fire guided rounds. Phase I testing of a guided unitary round (XM31) was completed on an accelerated schedule in March 2006. Due to an Urgent Need Statement, the guided unitary round was quickly fielded and used in action in Iraq. Lockheed Martin also received a contract to convert existing M30 Dual-Purpose Improved Conventional Munition (DPICM) GMLRS rockets to the XM31 unitary variant. The M31 GMLRS Unitary rocket transformed the M270 into a point target artillery system for the first time. Due to GPS guidance and a single 200 lb (91 kg) high-explosive warhead, the M31 could hit targets accurately with less chance of collateral damage while needing fewer rockets to be fired, reducing logistical requirements. The unitary warhead also made the MLRS able to be used in urban environments. The M31 had a dual-mode fuse with point detonation and delay options to defeat soft targets and lightly fortified bunkers respectively, with the upgraded M31A1 equipped with a multi-mode fuse adding a proximity airburst mode for use against personnel in the open; proximity mode can be set for 3 or 10 meters (9.8 or 32.8 ft) Height Of Burst (HOB). The GMLRS has a minimum engagement range of 15 km (9.3 mi) and can hit a target out to 70 km (43 mi), impacting at a speed of Mach 2.5. A German developmental artillery system, called the Artillery Gun Module, has used the MLRS chassis on its developmental vehicles. In 2012, a contract was issued to improve the armor of the M270s and improve the fire control to the standards of the High Mobility Artillery Rocket System (HIMARS). In June 2015, the M270A1 conducted tests of firing rockets after upgrades from the Improved Armored Cab project, which provides the vehicle with an enhanced armored cab and windows.

Ground Specifications
Crew 3
Engine 903-cu in (14.8-liter) liquid-cooled, 4-stroke, turbo-charged, V-8 diesel (500 hp)
Active Protection None
Max Speed 64.0 km/h
Range 483.0 km
Variants
M270 is the original version, which carries a weapon load of 12 rockets in two six-pack launch pod containers. This armored, tracked mobile launcher uses a stretched Bradley chassis and has a high cross-country capability.
M270 IPDS was an interim upgrade applied to a select number of launchers to provide the ability to fire the longer-range GPS-aided ATACMS Block IA, quick-reaction unitary and Block II missiles until sufficient M270A1 launchers were fielded.
M270A1 was the result of a 2005 upgrade program for the U.S. Army, and later on for several other states. The launcher appears identical to M270, but incorporates an improved fire control system (IFCS) and an improved launcher mechanical system (ILMS). This allows for significantly faster launch procedures and the firing of new types of munitions, including GPS guided missiles.
M270B1 is a British Army upgrade, similar to the A1, but it also includes an enhanced armor package, which gives the crew better protection against IED attacks.
M270C1 was an upgrade proposal from Lockheed Martin involving HIMARS Universal Fire Control System (UFCS) instead of IFCS
MARS2 / LRU is a European upgrade of M270 involving Germany, Italy and France. MARS2 is equipped with a new fire control system (EFCS - European Fire Control System) designed par Airbus Defense and Space. EFCS enables firing of M31, M31A1, M32, AT2 and 110 mm rockets, but not of M26, M26A1, and M30, so as to ensure full compliance with the Convention on Cluster Munitions.
M270D1 includes a new fire control system that allows for firing GPS-guided rockets, such as GMLRS and ATACMS. The update package consists of a new computer, locating device, GPS antenna, launch control unit, displays and remote control device. Current operators include United States, United Kingdom, Bahrain, and Finland.
System
Alternative Designation M270
Type Multiple Launch Rocket System (MLRS)
Composite The M270 multiple launch rocket system (MLRS), also known as the armored vehicle-mounted rocket launcher (AVMRL), consists of an M269 launcher loader module (LLM) bearing two six-cell rocket launch pods/containers (LP/C) mounted on an M993 carrier vehicle.
Crew 3 (section chief, gunner and driver) crew can fire entire load from cab and can reload MLRS without other help.
Chassis M993 carrier vehicle. The M993 is a modified M2 Bradley armored personnel carrier.
Displacement Time Less than 5 min
Emplacement Time Less than 5 min
Dimensions
Length 6.97 m
Width 2.97 m
Height, Elevated 5.93 m
Height, Traveling 2.62 m
Track Length on Ground 4.33 m
Track Width 0.53 m
Ground Clearance 0.43 m
Combat Weight 25,191 kg
Unloaded Weight 20,189 kg
Launch Pad Weight 2,270 kg
Automotive
Engine Name 1 x Cummins VTA-903
Engine Type 903-cu in (14.8-liter) liquid-cooled, 4-stroke, turbo-charged, V-8 diesel
Engine Power 500 hp at 2400 rpm
Power-to-Weight Ratio 19.85 hp/metric ton
Fuel Capacity 617 liters
Transmission General Electric HMPT-500 hydro-mechanical; 3 forward/1 reverse range (variable ratios)
Suspension torsion bar, 6 dual road wheels, front drive, rear idler, 2 shock absorbers, 4 return rollers
Maximum Speed 64 km/h
Maximum Range 483 km
Gradient 60 percent
Vertical Obstacle 1.00 m
Trench 2.29 m
Fording 1.10 m
Main Weapon System
System
Name M269 launcher loader module (LLM)
Type Launcher Loader Module
Caliber 227 mm
Number of Cells 12 ea
Elevation 60 deg (1,067 mils)
Elevation Rate 0.9 deg (15.5 mils)/sec
Traverse +/-194 deg (3,449 mils) each side of centerline
Rate of Fire less than one minute for 12 missiles
Effective Firing Range See Ammunition Types
Reload Time 4 min (M270) 3 min (M270A1)
Ammunition (Option 1)
Name M26 (Phase I)
Length 3.94 m
Diameter 227 mm
Weight 306 kg
Warhead 156 kg
Maximum Range 32 km
Basic Load INA
Ammunition (Option 2)
Name AT2 (Phase II)
Length 3.94 m
Diameter 227 mm
Weight 259 kg
Warhead 107 kg
Maximum Range 40 km
Basic Load INA
Ammunition (Option 3)
Name GMLRS
Length 3.94 m
Diameter 227 mm
Weight 302 kg
Maximum Range 60 km
Basic Load INA
Fire Control
Name Westinghouse Norden FCS
Computerized FCS Yes
Direct Fire Yes
Indirect Fire Yes
SRP/PDS Bendix stabilization reference package/position determining system (SRP/PDS)
Protection
Hull Armor The cab is protected against small-arms fire and shell fragments by aluminum armor and louvred windows. Some U.S. M270s are equipped with a Mk 19 40-mm automatic grenade launcher on the roof.
Applique Armor No
Explosive Reactive Armor No
Active Protection System No
NBC Protection overpressure protection
Smoke Equipment INA
EMP Hardened electronics
Details
Country of Origin United States
Category Rocket Artillery Systems
Land > Artillery > Rocket Artillery Systems
Filter Label
M
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
6.97 m
Width
2.97 m
Height
2.62 m
Weight
25191 kg
Operators (13)
United States
France
Germany
United Kingdom
Israel
Italy
Japan
Turkey
Bahrain
Egypt
Finland
Greece
Saudi Arabia
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