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BM-24 (Katyusha) Russian 240mm Multiple Rocket Launcher

BM-24

Multiple Launch Rocket System (MLRS)
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Basic Information
Name
BM-24 (Katyusha) Russian 240mm Multiple Rocket Launcher
Designation
BM-24
Alternate Designation
BM-24
Equipment Type
Multiple Launch Rocket System (MLRS)
Manufacturer
Date of Introduction
1947
Description

The BM-24 is a multiple rocket launcher designed in the Soviet Union. It is capable of launching 240mm rockets from 12 launch tubes. Versions of the BM-24 have been mounted on the ZIL-151 6x6 Truck chassis and the AT-S tracked artillery tractor, forming the BM-24T from the latter. Production began out of Automotive Factory no. 2 in 1947 Moscow. Israel operated one battalion, consisting of vehicles captured from Egypt in the Six-Day War. The battalion took part in the Yom Kippur War and the 1982 Lebanon War. The Soviet Army was equipped with BM-24 after WWII. The BM-24 multiple launch rocket system fired the powerful M-24F 240mm rockets, each carrying 27,4 kg of the explosive. In addition to the M-24F, the system could also fire the M-24FUD, having the lighter 18,4 kg shell, but with a longer 10600m range. The MS-24 and MS-24D, loaded with P-35 poison-gas, were also available. The system had 12 launch tubes located on a rotary frame, disposed on a stub pole at the vehicle rear. The lining and turning mechanisms were hand-driven. The cabin and fuel tanks were protected from rocket exhaust by steel skin plates. Two jacks were set against the soil before shooting to discharge the back axles springs and to stabilize the platform. The 95 hp engine permitted the BM-24 to reach a speed of 55km/h on the highway and to have a range of up to 600 km.

Ground Specifications
Crew 6
Engine Gasoline (109 hp)
Active Protection None
Range 430.0 km
Variants
BM-24 (8U31) Basic model, mounted on a ZiS-151 chassis.
BM-24M (2B3) Modified model, mounted on a ZIL-157 chassis
BM-24T Tracked model, mounted on an AT-S chassis
System
Alternative Designation BM-24
Type Multiple Rocket Launcher
Family INA
Crew 6 ea
Chassis ZiS-151 chassis
Displacement Time INA
Emplacement Time INA
Dimensions
Length 6.7 m
Width 2.3 m
Height 2.91 m
Weight, Combat 9,200 kg
Ground Pressure INA
Automotive
Engine Name 1 x Zil-151
Engine Type Gasoline Fueled Engine
Engine Power 109 hp
Maximum Range 430 km
Speed, Maximum Road 65 km/h
Speed, Average Cross INA
Speed Maximum Swim Not Amphibious
Fording Depth INA
Main Weapon System
System
Name M-24FUD Rockets
Types HE, Smoke, Chemical
Shell Weight 18.4 kg
Maximum Effective Range 10.6 km
Launch Tubes 12 ea
Elevation INA
Traverse INA
Basic Load 12 ea
Note Two jacks were set against the soil before shooting to discharge the back axles springs and to stabilize the platform.
Fire Control
Name INA
Computerized FCS No
Direct Fire INA
Indirect Fire Yes
Position Location System INA
Protection
Hull Armor INA
Applique Armor No
Explosive Reactive Armor No
Active Protection System No
Mine Clearing No
Self-Entrenching Blade No
NBC Protection INA
Smoke Equipment INA
Details
Country of Origin Russia
Category Rocket Artillery Systems
Land > Artillery > Rocket Artillery Systems
Filter Label
B
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
6.7 m
Width
2.3 m
Height
2.91 m
Weight
9200 kg
Operators (4)
North Korea
Algeria
Angola
Yemen
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