M270 Multiple Launch Rocket System

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M270 Multiple Launch Rocket System (MLRS)
M270 MLRS
Type	Rocket artillery
Place of origin	Multi-National
Service history
In service	Since March 31, 1983
Production history
Designer	Vought Corporation
Designed	1977
Manufacturer	Lockheed Martin
Produced	1980
Variants	M-270A1
Specifications
Weight	54,500 lbs
Length	22.4 ft
Width	9.8 ft
Height	8.5 ft
Crew	3
Rate of fire	Rockets - 12 in < 60 sec Missiles - 2 in 20 sec
Primary armament	M269 Launcher Loader Module
Engine	Cummins Diesel 400 hp
Operational range	300 miles
Speed	40 mph

The M270 Multiple Launch Rocket System (M270 MLRS) is a multiple rocket launcher, a type of rocket artillery.

The first rocket systems were delivered to the US Army in 1983. The system is in widespread use in the NATO countries and it has also been manufactured in Europe. Some 1,300 M270 systems have been manufactured, along with more than 700,000 rockets. The system has been used in the Gulf wars, where it proved itself as a practical and effective weapons system. The production of the M270 ended in 2003, when a last batch was delivered to the Egyptian army.

Contents 1 Overview 2 History 3 MRLS Rockets and Missiles 3.1 Selected Rocket specifications 4 Launcher specifications 5 Operators 6 References 7 See also 8 External links

[edit] Overview

The system is capable of firing guided and unguided projectiles to a distance of up to 42 km (26.1 miles). Firing modern munitions (such as the US Army Tactical Missile System - ATACMS) it is capable of reaching out to 300 km (186 miles) with the projectile reaching a maximal altitude of ~50 km (164,000 ft). The M270 is a very mobile unit, thus well suited for the so called shoot-and-scoot tactic: it can fire its rockets very rapidly and immediately move away to avoid the counter-battery fire.

MLRS was developed jointly by the United Kingdom, United States, Germany, and France. It was developed from the older General Support Rocket System (GSRS).

The rockets and ATACMS missiles are contained in interchangeable pods. Each pod contains six standard rockets or one guided ATACMS missile (the two types cannot be mixed). The launcher can hold two pods at a time, which it loads using an integrated crane. 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. The US Army is currently working on developing and fielding unitary (one large warhead instead of submunitions) rocket and ATACMS variants, as well as a guided rocket.

MLRS has recently been upgraded with 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 has already been fielded and used in action in Iraq.^[1] Lockheed Martin also received a contract to convert existing M30 DPICM GMLRS rockets to the XM31 unitary variant.^[2]

[edit] History

When first deployed with the US Army, the MLRS was used in a composite battalion consisting of 2 batteries of traditional artillery (howitzers) and one battery of MLRS SPLLs (self-propelled loader/launchers). The first operational organic or "all MLRS" battalion (6th Bn, 27th FA, Ft. Sill, OK) started training in the winter of 1985. Alpha Battery, 4/27th FA (MLRS) was deployed en masse to Peden Barracks at Wertheim, West Germany in April of that year. "Sudden Impact" as it was known by its members fired its first rounds in theater and was considered operational in June of that year. Two other firing batteries soon joined. 6/27th FA (MLRS) deployed in support of Operation Desert Shield in October 1990. A Btry 6/27th FA was the first ground unit to fire in support of Operation Desert Storm, firing a missile at approximately 00:40 (12:40am)January 18th. The 4/27th FA (MLRS) was deployed in support of Operation Desert Shield on Christmas Day 1990. It has since been used in numerous military engagements including the 2003 invasion of Iraq. Frightened Iraqi soldiers gave it the nickname "steel rain". In March 2007 the british ministry of defense decided to send a troop of MLRS to support ongoing operations in the southern province of Helmand, they will use newly developped guided munitions.

[edit] MRLS Rockets and Missiles

The M270 system can fire MFOM, MLRS Family Of Munition rockets and artillery missiles, which are manufacturered by a number of coutries. These include:

• M26 (United States) - Rocket with 644 M77 Dual-Purpose Improved Conventional Munitions (DPICM) sub-munitions, range of 23 km.
  • M26A1 (United States) - Extended Range Rocket (ERR), with range of 45 km and using improved M85 submunitions.
  • M26A2 (United States) - As M26A1, but using M77 submunitions.
• M27 (United States) - Completely inert training Launch Pod/Container to allow full loading cycle training.
• M28 (United States) - Training rocket. M26 with three ballast containers and three smoke marking containers in place of submunition payload.
  • M28A1 (United States) - Reduced Range Practice Rocket (RRPR) with blunt nose. Range reduced to 9 km.
• XM29 (United States) - Rocket with Sense and Destory Armor (SADARM) submunitions. Not standardized.
• M30 (United States) - Guided MRLS (GMRLS). A precision guided rocket, range 60—100 km, in pre-production, with a standard load of 404 M85 submunitions.
  • XM31 (United States) - Variant of the M30 with a unitary high-explosive warhead.
• XM135 (United States) - Rocket with binary chemical warhead (VX (nerve agent)). Not standardized.
• MGM-140A (United States) - Army Tactical Missile System (ATACMS). A large guided missile using the M270 launcher, with a variety of warheads.

Main article: MGM-140 ATACMS

• AT2 (Germany) - SCATMIN Rocket with 28 anti-tank mines and range of 38 km.

[edit] Selected Rocket specifications

• Caliber: 227 mm (8.94 in)
• Length: 3.94 m (12.93 ft)
• Motor: Solid-fuel rocket

• M26
  • Weight: 306 kg (675 lb)
  • Maximum range: 32 km (20 miles)
  • Warhead: 644 M77 DPICM submunitions

• M26A1/A2
  • Weight: 296 kg (650 lb)
  • Maximum range: over 45 km (28 miles)
  • Warhead:
    • M26A1 - 518 M85 DPICM submunitions
    • M26A2 - 518 M77 DPICM submunitions

• M30/XM31
  • Maximum range: over 45 km (28 miles)
  • Guidance: GPS/INS
  • Warhead:
    • M30 - 404 M85 DPICM submunitions
    • XM31 - 90 kg (200 lb) unitary HE

• AT2 SCATMIN
  • Weight: 254.46 kg
  • Maximum range: 39 km

• PARS SAGE-227 F
  • Weight: over 300 kg/160 kg
  • Maximum range: 70 km

[edit] Launcher specifications

• Entered Service: 1982 (US Army)
• First used in action: 1991 (First Gulf War)
• Crew: 3
• Weight loaded: 24,756 kg
• Length: m
• Width: m
• Height (stowed): m
• Height (max elevation): m
• Max road speed: 64 km/h
• Cruise range: 480 km
• Reload time: 8 minutes
• Engine: Turbo-charge 8 cylinder Detroit diesel
• Average unit cost: $2.3M ^[3]

[edit] Operators

•  Bahrain: Bahrain Army
•  Denmark: Royal Danish Army (no longer in service)
•  Finland: Finnish Army
•  France: French Army
•  Egypt: Egyptian Army
•  Germany: German Army
•  Greece: Hellenic Army
•  Israel: Israel Defense Forces
•  Italy: Italian Army
•  Japan: Japan Ground Self-Defense Force
•  Norway: Norwegian Army
•  South Korea: Republic of Korea Army
•  Turkey: Turkish Army
•  United Kingdom: British Army
•  United States: United States Army

[edit] References

[edit] See also

• M-26 artillery rocket
• Multiple rocket launcher

[edit] External links

• Lockheed US MLRS
• British MLRS
• Designation Systems
• Diehl BGT - German developer and manufacturer of GMLRS (site in English)