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WM-80 Chinese 273mm Multiple Rocket Launcher (MRL)

WM-80

Multiple Launch Rocket System (MLRS)
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Basic Information
Name
WM-80 Chinese 273mm Multiple Rocket Launcher (MRL)
Designation
WM-80
Alternate Designation
WM-80
Equipment Type
Multiple Launch Rocket System (MLRS)
Manufacturer
Date of Introduction
1995
Description

The WM-80 multiple launch rocket system was developed by China North Industries Group Corporation (NORINCO) based on the indigenous Type 83 273mm 4-tube artillery rocket system. The WM-80 did not enter PLA service, possibly due to the introduction of the more capable A-100 artillery rocket system. NORINCO has been promoting the weapon system to the export market and made one sale to Armenia in 1999. The WM-80 rocket system is composed of multiple rocket launchers, ammunition transporter/loader, fire command and control vehicles, and maintenance vehicles. The fire command and control is composed of a brigade/regiment command vehicle, battalion command vehicle, surveillance/spotting radar, and meteorological radar. A total of six launcher vehicles and six resupply vehicles would be attached to each battery. The standard combat unit is considered to be the battalion with the customer choosing his own Table Of Equipment (TOE) if they so wish. Fire-control and command duties throughout the brigade are accomplished by the use of an automatic distribution network. This consists of main computers located at the brigade, battalion, and battery HQ command levels with various terminals and radio/wire communications links to automatically distribute the data as directed.

Ground Specifications
Crew 5
Engine Diesel (525 hp)
Range 400.0 km
System
Alternate Designation WM-80
Type Multiple Rocket Launcher (MRL)
Caliber 273 mm
Quantity, Tubes 8 (2 rows of 4 tubes)
Chassis Taian TAS5380 8X8
Crew 5 ea
Displacement Time 3 to 5 min
Emplacement Time 3 to 5 min
Reload Time 5 to 8 min
Launch Rate, Full Salvo Time 8 rounds in 5 seconds
Launch Rate, Single Rocket Interval 0.5 seconds per rocket
Launcher Drive Electric
Loader Type Manual
Elevation -20/+60 deg
Traverse 40 deg
Traverse, Right 20 deg
Traverse, Left 20 deg
Dimensions
Height 3.3 m
Length, Chassis Overall 9.55 m
Width 3.06 m
Weight, Combat 34 tons
Automotive
Engine Name INA
Engine Type Diesel
Engine Power 525 hp
Range 400 km
Speed, Maximum Cross-Country INA
Speed, Maximum Off-Road INA
Speed, Maximum On-Road 70 km/h
Traversable Slope 35 degrees
Communications
Radio
Name INA
Note Wire-link or radio communications systems can be used to communicate firing data
Ammunition
Rocket Caliber 273 mm
Rocket Length 4,582 mm
Rocket Weight 505 kg
Warhead Weight 150 kg
Circular Error Probable (CEP) 2% of range
Maximim Range 80 km
Max Ord Alititude 31,000 m (at max range of 80km)
Minimum Range 34 km
Max Time of Flight 165 sec (at max range of 80km)
Rocket Stabilization The rocket is stabilized by tail fins and high-speed spin generated by a spin motor
High-Explosive (HE) The HE blast warhead contains 34kg of explosive that can be activated by a WJ-6A mechanical impact fuse or a MD-23A electronic proximity fuse
Submunitions Contains 380 bomblets with a HEAT warhead
Armor Penetration Up to 100 mm
Fire Control System
Collimator INA
Computerized Yes
Note There is also a standard optical sighting system on the left side of the launcher as an emergency back up. If required the rockets can also be launched by remote control away from the launcher.
Protection
NBC Protection No
Self-Entrenching Blade No
Smoke Equipment No
Details
Country of Origin China
Category Rocket Artillery Systems
Land > Artillery > Rocket Artillery Systems
Filter Label
W
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
Width
3.06 m
Height
3.3 m
Weight
34000 kg
Operators (3)
China
Armenia
Jordan
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