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9K52 Luna-M
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9K52 Luna-M
The 9K52 Luna-M (Russian: Луна, English: Moon; NATO reporting name: Frog-7) is a Soviet short-range artillery rocket system which fires unguided and spin-stabilized 9M21 rockets. It was originally developed in the 1960s to provide divisional artillery support using tactical nuclear weapons but gradually modified for conventional use. The 9K52 was succeeded by the OTR-21 Tochka.
Originally called the 3R-11 and 9R11, the 9M21 is a solid fuel rocket, with four off-angle vernier chambers immediately behind the warhead section. When the main engine section ignites, the verniers activate to start spinning the rocket, to improve stability and accuracy. At range, the 9M21 has a nominal CEP (circular error probable) of 400 meters. Western intelligence estimated that its CEP at maximum range was 500 to 700 meters. Russian sources admit the likely impact point could fall anywhere within an area 2.8 kilometers in depth from range error, and 1.8 kilometers in width in azimuth error.
The initial 3R-11 rocket, known also by its military designation R-65 (NATO: Frog-7A), measures 8,900 mm in length. It was replaced in 1968 with an improved R-70 (NATO: Frog-7B) which measures 9,400 mm. This new variant allows for switching warhead sections and the addition of air brakes at the rear of the rocket, lowering the minimum range to 15 km (9.3 mi).
The rocket is mounted on a transporter erector launcher (TEL), designated 9P113. Based on the ZIL-135LM 8x8 truck, it features a large hydraulic crane to allow faster reloading. The 9T29 transporter, also based on the ZIL-135RTM chassis, can carry up to three 9M21 rockets.
In addition to its inaccuracy, the fact that the rocket was exposed to the weather was another drawback to the system, particularly when equipped with temperature-sensitive nuclear ordnance. In the early 1960s, the Soviets experimented with a modified 9P113 launch vehicle with a fully-enclosed superstructure and launch roof. This did not solve the issue entirely, necessitating the development of the Tochka.
In Soviet service, the Luna-M was organized into battalions to provide divisions with rocket artillery support. Each battalion was organized with a headquarters battery and two firing batteries. Total complement included 20 officers, 160 enlisted personnel, four 9P113 launchers and, on average, seven rockets per launcher.
The headquarters battery numbered about 80 personnel and provided the battalion with command and logistical support. Vehicles included 4 9T29 transporter vehicles, a 9T31M1 crane vehicle (Ural-375D), an RM-1 maintenance complex (3 ZIL-157s), an RVD-1 optical maintenance vehicle (Ural-375D) and a PKPP maintenance/check vehicle (ZIL-131).
Each firing battery was organized with a headquarters, a meteorological section, a survey section, and two firing sections. The headquarters included a 9S445M command vehicle: a GAZ-66 truck with attached shelter containing fire control computer, radios and telephones. The meteorological section operated the RVS-1 Malakhit and a RMS-1 meteorological radar in the 1970s. They later upgraded to a RMS-1 End Tray radar, supported by an auxiliary power unit, each towed by a GAZ-66. The survey section used a GAZ-69TM/TMG/TMG-2, GAZ-66T or UAZ-452T for launch site preparation. Each firing section consisted of a single 9P113.
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9K52 Luna-M
The 9K52 Luna-M (Russian: Луна, English: Moon; NATO reporting name: Frog-7) is a Soviet short-range artillery rocket system which fires unguided and spin-stabilized 9M21 rockets. It was originally developed in the 1960s to provide divisional artillery support using tactical nuclear weapons but gradually modified for conventional use. The 9K52 was succeeded by the OTR-21 Tochka.
Originally called the 3R-11 and 9R11, the 9M21 is a solid fuel rocket, with four off-angle vernier chambers immediately behind the warhead section. When the main engine section ignites, the verniers activate to start spinning the rocket, to improve stability and accuracy. At range, the 9M21 has a nominal CEP (circular error probable) of 400 meters. Western intelligence estimated that its CEP at maximum range was 500 to 700 meters. Russian sources admit the likely impact point could fall anywhere within an area 2.8 kilometers in depth from range error, and 1.8 kilometers in width in azimuth error.
The initial 3R-11 rocket, known also by its military designation R-65 (NATO: Frog-7A), measures 8,900 mm in length. It was replaced in 1968 with an improved R-70 (NATO: Frog-7B) which measures 9,400 mm. This new variant allows for switching warhead sections and the addition of air brakes at the rear of the rocket, lowering the minimum range to 15 km (9.3 mi).
The rocket is mounted on a transporter erector launcher (TEL), designated 9P113. Based on the ZIL-135LM 8x8 truck, it features a large hydraulic crane to allow faster reloading. The 9T29 transporter, also based on the ZIL-135RTM chassis, can carry up to three 9M21 rockets.
In addition to its inaccuracy, the fact that the rocket was exposed to the weather was another drawback to the system, particularly when equipped with temperature-sensitive nuclear ordnance. In the early 1960s, the Soviets experimented with a modified 9P113 launch vehicle with a fully-enclosed superstructure and launch roof. This did not solve the issue entirely, necessitating the development of the Tochka.
In Soviet service, the Luna-M was organized into battalions to provide divisions with rocket artillery support. Each battalion was organized with a headquarters battery and two firing batteries. Total complement included 20 officers, 160 enlisted personnel, four 9P113 launchers and, on average, seven rockets per launcher.
The headquarters battery numbered about 80 personnel and provided the battalion with command and logistical support. Vehicles included 4 9T29 transporter vehicles, a 9T31M1 crane vehicle (Ural-375D), an RM-1 maintenance complex (3 ZIL-157s), an RVD-1 optical maintenance vehicle (Ural-375D) and a PKPP maintenance/check vehicle (ZIL-131).
Each firing battery was organized with a headquarters, a meteorological section, a survey section, and two firing sections. The headquarters included a 9S445M command vehicle: a GAZ-66 truck with attached shelter containing fire control computer, radios and telephones. The meteorological section operated the RVS-1 Malakhit and a RMS-1 meteorological radar in the 1970s. They later upgraded to a RMS-1 End Tray radar, supported by an auxiliary power unit, each towed by a GAZ-66. The survey section used a GAZ-69TM/TMG/TMG-2, GAZ-66T or UAZ-452T for launch site preparation. Each firing section consisted of a single 9P113.
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