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M142 (HIMARS) American Artillery Rocket System

M142 HIMARS

Wheeled 6x6 Multiple Launch Rocket System (MLRS)
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Basic Information
Name
M142 (HIMARS) American Artillery Rocket System
Designation
M142 HIMARS
Alternate Designation
M142 HIMARS
Equipment Type
Wheeled 6x6 Multiple Launch Rocket System (MLRS)
Manufacturer
Date of Introduction
2000
Description

The M142 High Mobility Artillery Rocket System (HIMARS) is a light multiple rocket launcher developed in the late 1990s for the United States Army, mounted on a standard Army M1140 truck frame. The HIMARS carries six rockets or one MGM-140 ATACMS missile on the U.S. Army's new Family of Medium Tactical Vehicles (FMTV) five-ton truck, and can launch the entire Multiple Launch Rocket System Family of Munitions (MFOM). HIMARS ammunition is interchangeable with the MLRS M270A1, however it is only able to carry one pod rather than the standard two for the M270 and A1 variants. The launcher is C-130 transportable. The chassis was produced by BAE Systems Mobility & Protection Systems (formerly Armor Holdings Aerospace and Defense Group Tactical Vehicle Systems Division), the OEM of the FMTV; however, since 2010, the M1140 has been produced by the Oshkosh Corporation by their Defense division. The rocket launching system is produced by Lockheed Martin Missiles & Fire Control.

Ground Specifications
Crew 3
Engine 6.6 liter, 6 cylinders, turbocharged diesel (330 hp)
Active Protection None
Max Speed 64.0 km/h
Range 484.0 km
System
Alternative Designation M142 HIMARS
Type Wheeled 6x6 Multiple Launch Rocket System (MLRS)
Crew 3 (section chief, gunner and driver)
Chassis Oshkosh Defense- FMTV 6 × 6; however, the HIMARS launcher can be fitted onto other 6 × 6 tactical truck chassis types with similar payload capabilities.
Displacement Time Less than 3 min
Emplacement Time Less than 3 min
Dimensions
Length 7.7 m
Width 2.4 m
Height 2.91 m
Ground Clearance 0.56 m
Combat Weight 15,873 kg
Automotive
Engine Name Caterpillar 3116 ATAAC
Engine Type 6.6 liter, 6 cylinders, turbocharged diesel
Engine Power 330 hp at 2600 rpm
Suspension torsion bar, 6 dual road wheels, front drive, rear idler, 2 shock absorbers, 4 return rollers
Maximum Speed 64 km/h
Maximum Range 484 km
Amphibious No
Fording 1.5 m (with preparation)
Gradient 60 percent
Main Weapon System
Launcher
Name M269 launcher loader module (LLM)
Type Launcher Loader Module
Caliber 227 mm
Number of Cells 6 ea
Elevation 60 deg (1,067 mils)
Elevation Rate 0.9 deg (15.5 mils)
Traverse +/-194 deg (3,449 mils) each side of centerline
Rate of Fire less than 30 seconds for 6 missiles
Reload Time 4 min
Ammunition (Option 1)
Name M26
Length 3.94 m
Diameter 227 mm
Weight 306 kg
Warhead 156 kg
Maximum Range 32 km
Basic Load 6 ea
Ammunition (Option 2)
Name AT2
Length 3.94 m
Diameter 227 mm
Weight 259 kg
Warhead 107 kg
Maximum Range 40 km
Basic Load 6 ea
Ammunition (Option 3)
Name GMLRS
Length 3.94
Diameter 227 mm
Weight 259 kg
Warhead 302 kg
Maximum Range 60 km
Basic Load 6 ea
Ammunition (Option 4)
Name MGM-140 ATACMS
Length 4.0 m
Diameter 610 mm
Weight 270 kg
Warhead 120 kg
Maximum Range 128 km
Basic Load 1 ea
Fire Control
Name Lockheed Martin Universal Fire Control System (UFCS)
Computerized FCS Yes
Direct Fire Yes
Indirect Fire Yes
Note In a typical mission, a command and control post would transmit the selected target data via a secure data link to the HIMARS on-board launch computer. The computer then aims the launcher and provides prompt signals to the crew to arm and fire a pre-selected number of rounds. The launcher can aim at a target in just 16 seconds. It is possible for the crew to select pre-programmed multiple mission sequences, which have been stored in the computer.
Protection
Cab Armor The cab is protected against small-arms fire and shell fragments by aluminum armor and louvred windows.
Applique Armor No
Explosive Reactive Armor No
Active Protection System No
NBC Protection No
Smoke Equipment No
EMP INA
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
7.7 m
Width
2.4 m
Height
2.91 m
Weight
15873 kg
Operators (8)
United States
Ukraine
Poland
Jordan
Romania
Singapore
United Arab Emirates
CFE Treaty
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