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M270 MLRS


Multiple Launch Rocket System (MLRS)


United States | 1983



"The M270 MLRS was introduced in the latter half of the Cold War, adding lethal projected firepower on a modified chassis of the M2 Bradley IFV."

Power & Performance
Those special qualities that separate one land system design from another. Performance specifications presented assume optimal operating conditions for the M270A1 MLRS Multiple Launch Rocket System (MLRS).
1 x Cummins VTA-903T V-8 turbocharged diesel engine developing 600 horsepower @ 2,600rpm.
Installed Power
40 mph
64 kph
Road Speed
300 miles
483 km
Range
Structure
The physical qualities of the M270A1 MLRS Multiple Launch Rocket System (MLRS).
3
(MANNED)
Crew
23.0 ft
7 meters
O/A Length
9.8 ft
3 meters
O/A Width
8.5 ft
2.6 meters
O/A Height
61,729 lb
28,000 kg | 30.9 tons
Weight
Armament & Ammunition
Available supported armament, ammunition, and special-mission equipment featured in the design of the M270 MLRS Multiple Launch Rocket System (MLRS).
12 x 227mm Solid-Fuel Rockets / Missiles.
AMMUNITION:
12 x Tactical Rockets or Missiles (various warhead types supported, guided and unguided).
Variants
Notable series variants as part of the M270 MLRS family line.
M270 - Initial production models
M270A1 - Modernization program that includes cleaning/refurbishing existing rockets, GPS navigation system, update fire control system and upgraded launch system.
M270B1 - British Army upgrade to M270A1 standard with additional armor protection.
M270 IPDS - Interim model bridging original mark with A1 marks. Support for ATACMS guided munitions.


Authored By: Staff Writer | Last Edited: 04/21/2021 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.

The M270 MLRS (Multiple Launch Rocket System) is an American-developed battlefield support weapon produced by Lockheed Martin Vought. It is based on the lengthened chassis of the M2 Bradley Infantry Fighting Vehicle (IFV) to form the M993 Multiple Launch Rocket System carrier unit to which the installed launcher component is the M270. The completed system yields an impressive level of firepower for area suppression and sees the launcher house twelve tactical battlefield rockets or missiles with varying warhead types available. Initially taken on by the U.S. Army in 1982, the M270 did not see its formal baptism of fire until the 1991 Gulf War where it proved successful in its role. Today (2014), the M270 still represents the U.S. Army's primary ground-based rocket-launching platform

The M270 vehicle sports an armored cab at the front of the hull with the positional launch pod container fitted over the rear section. The launch pod consists of 2 x 6 holders. A typical operating crew is three and these personnel sit protected in the cab during action. As with the M2 Bradley vehicle, the M270 is compact enough to be air transportable in the cargo hold of a Lockheed C-5 Galaxy or Boeing C-17 Globemaster heavy-lift transport. The M270 can launch its payload through either "ripple fire" or "full fire". Ripple fire will fire the tactical payload off one rocket at a time for a staggered result at the target area. Full fire sends the entire ordnance load skyward in seconds, the rockets set to arrive on target at the same time. As with the storied multiple rocket projectors of World War 2 (1939-1945), this makes the M270 a terrifyingly effective psychological weapon as well as a tactical one.

The M270 typically is arranged to fire the standard M26 tactical rocket. This munition features a 32 kilometer range and disperses some 644 submunitions over the target area. Other munitions include the modified M26A1 and M26A2 Extended Range (ER) variants, ATACMS Block I, chemical projectiles, and practice rockets (the latter for training purposes). Guided munitions support was introduced in 2006. Additional modernization followed in 2012.

The vehicle is driven by a Cummins VTA-903T V-8 turbocharged, diesel-fueled engine of 600 horsepower output. This is mated to a Crossdrive turbo electronically-controlled transmission system. Operational range reaches 400 miles on road at speeds up to 40 miles per hour. The running gear consists of six road wheels to a hull side with the drive sprocket at front and track idler at rear. Two track return rollers are featured.

Design work on the M270 began in 1977 and production spanned from 1980 to 2003. Variants have included the original M270 vehicles followed by the upgraded M270 IPDS (ATACMS support). This marked bridged the gap between the original A1 models. The upcoming M270A1 mark was a 2005 upgrade program with an improved Fire Control System (FCS) as launcher unit.

Beyond its service with the U.S. Army, the M270 has been adopted by the forces of Bahrain, Denmark, Egypt, France, Finland (as the "298 RsRakH"), Germany (as the "MARS"), Greece, Israel, Italy, Japan, Netherlands, Norway, South Korea, Turkey, and the United Kingdom. Denmark and Norway have since retired their M270 stock.

UK models were upgraded to the M270A1 form under the M270B1 designation. This project included improved armor protection not seen in the A1 upgrade.

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Operators
Global customers who have evaluated and/or operated the M270 MLRS. Nations are displayed by flag, each linked to their respective national land systems listing.

Total Production: 1,730 Units

Contractor(s): Lockheed Martin Vought - USA
National flag of Bahrain National flag of Denmark National flag of France National flag of modern Germany National flag of Greece National flag of Israel National flag of Italy National flag of modern Japan National flag of the Netherlands National flag of Norway National flag of South Korea National flag of Turkey National flag of the United States

[ Bahrain; Denmark; France; Germany; Greece; Israel; Italy; Japan; South Korea; Netherlands; Norway; Turkey; United States ]
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