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2K6 Luna (FROG-3) Russian Medium-Range Artillery Rocket System

2K6 Luna

Multiple Launch Rocket System (MLRS)
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Basic Information
Name
2K6 Luna (FROG-3) Russian Medium-Range Artillery Rocket System
Designation
2K6 Luna
Alternate Designation
2K6 Luna; NATO: FROG-3
Equipment Type
Multiple Launch Rocket System (MLRS)
Manufacturer
Soviet Union - SKB-221
Date of Introduction
1960
Description

The Russian FROG-3 [Free Rocket Over Ground], FROG-4, and FROG-5 are three variants of a single unguided, spin-stabilized, solid-fuel rocket. The 2K6 Luna (English: moon) is a Soviet short-range artillery rocket complex. Luna rockets were solid-fuel, unguided, and spin-stabilized. "2K6" is its GRAU designation. Its NATO reporting names are FROG-3 (with 3R9 missile) and FROG-5 (with 3R10 missile). From 1965, the 2K6 Luna was replaced by the far more successful 9K52 Luna-M, which was known in the West as the FROG-7. One of the first Soviet tactical missile systems with unguided missiles equipped with nuclear warheads. Intended for manning missile divisions of the tank and motorized rifle divisions, was to be used as a means of clearing in the offensive zone of the compound. It has been developed since 1953, launched in full-scale design in 1956, and has been tested since 1958, and entered service in 1960. The developer was the Moscow NII-1 (now the Moscow Institute of Heat Engineering, the creators of Topol, Yars and Maces). The Luna system was developed in NII-1 in 1953, under the supervision of N. P. Mazurov. Luna followed the earlier designs 2K1 Mars and 2K4 Filin. While NII-1 was responsible for the rocket, the launch and transporter-loader vehicles were designed by TsNII-58. The initial system name was S-125A "Pion". In 1957 the prototypes of the launch vehicle (SPU S-123A on Ob'yekt 160 chassis), the transponder (TZM S-124A on Ob'yekt 161 chassis), and the 3R5 rocket were ready for evaluations. These were carried out in 1958 in Kapustin Yar and in 1959 in the Transbaikal Military District. As a result of these evaluations, it was decided to abandon the TZM, to improve the SPU and to redesign the rocket. This led to the development of the 3R9 and 3R10 rockets. The decision to start series production was taken on 29 December 1959. The first 5 systems were ready in January 1960 after which the state acceptance trials were carried out until March of that same year. In 1960 the Luna system entered service with the Soviet Army where it remained until 1982. From 1960 till 1964, a total of 432 SPU 2P16s was produced. In the first year alone, 80 launch vehicles and 365 rockets were finished. The missile complex consisted of the launch vehicle SPU 2P16 (Ob'yekt 160), based on a modified PT-76B chassis with return rollers and fitted with a launch rail, elevation mechanism, stabilizing jacks, and a generator. Combat weight was 18 t; the rocket 3R9 with conventional HE warhead 3N15 and with a range of 12 to 44.6 km, the rocket 3R10 with a 400 kg nuclear warhead 3N14 and with a range of 10 to 32.1 km; a missile transporter 2U663 based on the ZiL-157V with 2 missiles; a vehicle 2U662 to transport and store nuclear warheads; a mobile crane ADK K52 (on MAZ-502), ADK K61 (on MAZ-200) or 9T31 (on Ural-375); sets of maintenance vehicles PRTB-1, 2U659, etc.; control and command vehicle PU-2 and a training set with training rocket PV-65 or 3R11 with training warhead 3N16.

Ground Specifications
Crew 5
Mobility Type Tracked
Main Weapon Launch rail for tactical rocket
Active Protection None
Range 44.7 km
Variants
9M21B Nuclear-armed variant, fitted with a 500 kg (1,213-lb) warhead.
9M21G This variant is fitted with a 390 kg (860-lb) warhead.
Laith-90 Iraqi version with increased range (90 km) and submunition warhead.
System
Alternative Designation 2K6 Luna; NATO: FROG-3
Type Medium-Range Artillery Rocket System
Manufacturer Soviet Union - SKB-221
Family 9K52
Crew 5 ea
Missile Complex The missile complex consisted of 1. the launch vehicle SPU 2P16 (Ob'yekt 160), based on a modified PT-76B chassis with return rollers and fitted with a launch rail, elevation mechanism, stabilizing jacks and a generator. Combat weight was 18 t; 2. the rocket 3R9 with conventional HE warhead 3N15 and with a range of 12 to 44.6 km, 3. the rocket 3R10 with a 400 kg nuclear warhead 3N14 and with a range of 10 to 32.1 km; 4. a missile transporter 2U663 based on the ZiL-157V with 2 missiles; 5. a vehicle 2U662 to transport and store nuclear warheads; 6. a mobile crane ADK K52 (on MAZ-502), ADK K61 (on MAZ-200) or 9T31 (on Ural-375); sets of maintenance vehicles PRTB-1, 2U659 etc.; 7. control and command vehicle PU-2 and 8. a training set with training rocket PV-65 or 3R11 with training warhead 3N16.
Displacement Time 5 min
Emplacement Time 5 min
Dimensions (2P16 Launch Vehicle)
Length, without Missile 7.95 m
Width 3.13 m
Height 2.92 m
Weight, Combat Load 17.3 tons
Weight, without Missile 15.1 tons
Ground Pressure 0.6 kg/cm²
Automotive (2P16 Launch Vehicle)
Engine Name V-6B
Engine Type 6-cylinder diesel
Engine Power 235 hp at 1.800 rpm
Power-to-Weight Ratio 14 hp/t
Transmission Manual, 4 forward, 1 reverse
Suspension 6-cylinder diesel
Maximum Speed, On-Road 40 km/h with rocket on road
Maximum Speed, Off-Road 16 - 18 km/h with rocket off road
Range 165 - 200 km on road
Gradient INA
Vertical Obstacle 1 m
Trench 2.8 m
Fording Amphibious
Main Weapon System
Transporter Erector Launcher (TEL)
Name 2P16 Launch Vehicle
Type Launch rail for tactical rocket
Elevation +60°
Traverse 5° left, 5° right
Missile (Option 1)
Name 3R9 Rocket
Type Artillery rocket, conventional warhead
Length 9.1 m
Diameter 415 mm
Wingspan 1.0 m
Warhead Weight 358 kg
Weight 2,155 kg
Warhead Type 3N15 HE-Fragmentation
Guidance System None, free flight rocket
Propulsion 1.2 to 2.0 km
Maximum Speed 767 m/s
Maximum Range 44.65 km
Minimum Range 12 km
Basic Load 1 x R39 Missile
Missile (Option 2)
Name 3R10 Rocket
Type Artillery rocket, nuclear warhead
Length 10.69 m
Diameter, Rocket Body 415 mm
Diameter, Warhead Section 540 mm
Wingspan 1.0 m
Warhead Weight 503 kg
Weight 2,287 kg
Warhead Type 3N14 nuclear warhead
Guidance System None, free flight rocket
CEP 1.2 to 2.0 km
Fuze 3A17 or 3A18 proximity fuse for airburst detonation
Propulsion Solid propellant rocket motor
Maximum Speed Over 700 m/s
Maximum Range 32.2 km
Minimum Range 10 km
Basic Load 1 x 3R10 Rocket
Fire Control
Name INA
Computerized FCS Yes
Protection
Hull Armor Steel, welded. 6 to 10 mm
Applique Armor INA
Explosive Reactive Armor No
Active Protection System No
Mine Clearing No
Self-Entrenching Blade No
NBC Protection INA
Smoke Equipment No
Details
Country of Origin Russia
Category Rocket Artillery Systems
Land > Artillery > Rocket Artillery Systems
Filter Label
2
Classification
Domain
Ground
Equipment Status
Active
Dimensions
Length
7.95 m
Width
3.13 m
Height
2.92 m
Weight
17300 kg
Operators (11)
Russia
Ukraine
North Korea
Soviet Union
Belarus
Afghanistan
Algeria
Cuba
Libya
Syria
Yemen
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