Munitions / Anti-tank missiles / 9K120 Ataka
9K120 Ataka
General Facts
- TYPE
Anti-tank missile - ORIGIN
USSR
- NICKNAMES
AT-9 Spiral-2 (NATO reporting name)
Ataka (system nickname) - DESIGNED
Late 1980s? - DESIGNER
Kolomna design bureau - PRODUCTION
1992 - present - PRODUCERS
Russia - NPO Mashinostroyenie
- QUANTITY
Unknown - UNIT COST
Unknown - CHARACTERISTICS
Good peneration
Various warhead available
High velocity and good range
No full launcher compatibility with 9K114
Introduction
The 9K120 Ataka is an anti-tank missile system of Soviet origin. It was developed in the late 1980s and is operational since the early 1990s. The system is called 9K120 Ataka and is missile is known as the 9M120. In the West the NATO reporting name AT-9 Spiral-2 is commonly used. The design is based on the earlier 9K114 Shturm (AT-6 Spiral), but performs better in penetration, accuracy and velocity.
Design
The overall design is similar to the older 9M114 missile with the tandem warhead located at the front, followed by the guidance section with small control vanes, the solid fuel sustainer and the small booster stage at the rear. The missile is stored and launched from a plastic container. The guidance is SACLOS and a VHF radio command link is used. Besides the missile the 9K120 system consists of a sighting and guidance system.
Firepower
The 9M120 is a powerful anti-tank missile with much improved performance over the older 9M114. The maximum range is 6 km for the 9M120 and the tandem warhead provides a penetration of 800 mm. In the improved 9M120M these figures are 8 km and 900 mm respectively. The accuracy is reported to be better than the older 9M114 system. A thermobaric and anti-helicopter version are available.
Platforms
The Ataka-V is for airborne use and the 9M120 is mainly used on the Mi-28 helicopter. It is also installed on some Mi-24 and Mi-17 upgrades. A vehicle and ship launched version, the Ataka-T, is also developed but has not been produced yet.
Users
The 9M120 is in Russian use and has been exported to several nations. At this moment it is used only on helicopters. The 9K120 Ataka is in fierce competition with the newer 9K121 Vikhr (AT-16 Scallion) system.
9M120
9M120: Original missile with tandem HEAT warhead for use against tanks. NATO reporting name AT-9 Spiral-2.
9M120M: Improved 9M120 with longer range and warhead with improved penetration.
9M120F: Version with thermobaric warhead for use against buildings and fortified positions. The F stands for Fugasnaya, which translates to high explosive.
9A220O: Anti-helicopter version of the 9M120 with expanding rod warhead. A warhead type that is usually used on dedicated air to air missiles. It retains the radio command guidance. Also known as 9M120O.
Type | Anti-tank missile |
---|---|
Diameter | 0.130 m body, 0.36 m wingspan |
Length | 1.83 m |
Weight | 48.5 kg |
Guidance | Radio command guidance |
---|---|
Warhead | Tandem HEAT shaped charge, 800 mm RHA after ERA |
Propulsion | Solid propellant rocket motor |
Speed | 550 m/s maximum |
Range | 400 m minimum, 5.8 km maximum |
---|---|
Altitude | Up to 4 km launch altitude |
Engagement envelope | - |
Remarks | - |
Type | Anti-tank missile |
---|---|
Diameter | 0.130 m body, 0.36 m wingspan |
Length | 1.8 m |
Weight | 49.2 kg |
Guidance | Radio command guidance |
---|---|
Warhead | Tandem HEAT shaped charge, 900 mm RHA after ERA |
Propulsion | Solid propellant rocket motor |
Speed | 550 m/s maximum |
Range | 800 m minimum, 8 km maximum |
---|---|
Altitude | Up to 4 km launch altitude |
Engagement envelope | - |
Remarks | - |
Type | Anti-tank missile |
---|---|
Diameter | 0.130 m body, 0.36 m wingspan |
Length | 1.6 m |
Weight | 49.5 kg |
Guidance | Radio command guidance |
---|---|
Warhead | Thermobaric warhead, 9.5 kg TNT equivalent |
Propulsion | Solid propellant rocket motor |
Speed | 550 m/s maximum |
Range | about 6 km |
---|---|
Altitude | Up to 4 km launch altitude |
Engagement envelope | - |
Remarks | - |
Type | Air to air missile |
---|---|
Diameter | 0.130 m body, 0.36 m wingspan |
Length | 1.6 m |
Weight | ? |
Guidance | Radio command guidance |
---|---|
Warhead | Expanding rod warhead with proximity fuze |
Propulsion | Solid propellant rocket motor |
Speed | 550 m/s maximum |
Range | about 6 km |
---|---|
Altitude | Up to 4 km launch altitude |
Engagement envelope | - |
Remarks | - |