ATAKA-T guided weapon system
Purpose:
Designed to defeat stationary and moving fielded and future main battle tanks, other armoured (IFVs, APCs) and small-size (like pillboxes and bunkers) targets, fortified assets, manpower under cover and in the open as well as aerial low-level targets flying at speeds of up 400 km/h in the day- and night-time and surface small-displacement vessels.
The ATAKA-T guided weapon system (GWS) (industrial code B07S1) is intended for installation in turrets and fighting compartments of various combat vehicles based on a tank chassis (e.g., tank support combat vehicle (TSCV), BMPT[TSCV]-72), IFVs, APCs, tractors, and other military trucks, ship-borne mounts, including those of foreign origin.
Components:
The GWS is composed of system equipment, combat equipment, maintenance facilities, training aids and equipment:
- B07S1.01.000 launcher;
- VIAM.461112.001 ground-based control equipment;
- 9M120-1 antitank guided missile;
- 9M120-1F guided missile;
- 9M120-1F-1 guided missile;
- 9M120-1 PRAKT practice missile;
- Group SPTA kits for GWS components;
- 9M120 MAKET dummy article;
- 242-EDM.000 electrical, weight and size, data recording dummy;
- 199.PK.200 gauge.
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Ataka-T GWS specifications |
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Parameter |
Value |
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Missile guidance |
Semiautomatic laser beam riding |
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Laying angles for 9M120-1 missile: - in azimuth, deg. - in elevation, deg. |
360 (due to turret rotation) From minus 10 to plus 25 |
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Firing range of 9M120-1 missile, km |
From 0.4 to 6.0 |
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Target altitude with reference to carrier datum |
From 0.0 to 2.0 (maximum target altitude is ensured over range of 3.3±0.5 km) |
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Number of targets engaged simultaneously |
1 |
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Missile launch mode |
Consecutive |
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Rate of fire, rounds./min. |
3-4 |
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Selection of missiles by warhead type |
Provided |
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Armour penetration behind ERA |
800, minimum |
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Time of flight to 5 km, s |
14.5, max. |
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Average flight speed |
Supersonic |
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Reaction time (minimum time for GWS to launch missile after achieving fully operational state), s |
Less than 1.2 |
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Number of missiles loaded on launcher, pcs. |
Up to 4 |
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Time for manual loading/unloading of one launcher guide, s |
30, max. |
Requirements for Ataka-T GWS carrier
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Specifications of carrier's fire control system required for appropriate B05S011 GWS operation |
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Parameter |
Value |
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Misalignment between axis of zero commands of information-field far-range channel and line of sight of optical channel, second of arc |
30.0, max. |
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Misalignment of line of sight of IIR-channel narrow field with respect to optical channel, second of arc |
30.0 max. |
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Laying angles of line of sight (LOS), deg. - up - down |
30.0, min. 10.0, min. |
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Maximum available angular rate of LOS laying, deg./s |
4.0, min. |
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Target centre LOS tracking error, mils - for target range of 5000 m - for target range of 50 m |
0.1, max. 0.5, max. |
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Launcher stabilization error over entire range of launcher laying, minutes of arc - for stationary target - for moving target |
10.0, max. 20.0, max. |
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Maximum launcher slew rate, deg./s - yaw - pitch |
6.0, min. 6.0, min. |
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CV speed, incl. on rough terrain, with operating GWS, km/h |
65, max. |
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Missile flight mode |
- LOS flight; - 4 to 8 meters above LOS for DUST firing mode to ranges between 1500 and 5500 meters |
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Initial missile flight mode when carrier FCS is switched over to GWS mode prior to range finding (set by carrier FCS) |
LOS flight |
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Requirements for target range finding by carrier equipment: - for missile's LOS flight mode
- for missile's above-LOS flight mode |
- when initial target range is automatically set to 6000 meters, no range finding is required before launch; - target range must be measured before missile launch within ± 50 meters |
KBM R&P Corp., JSC, is the manufacturer of 9M120-1, 9M120-1F, 9M120-1F-1 missiles and B07S1.01.000 launchers (versions 1 and 2) and renders services for the guided weapon system support.
B07S1.01.000 launcher
The B07S1.01.000 launcher is used to mount, secure, and launch 9M120-1, 9M120-1Ф, 9M120-1Ф-1 guided missiles.
The B07S1.01.000 launcher includes the following components:
Version 1:
- B07S1.01.150 left-side launch module;
- B07S1.01.160 right-side launch module;
- B07S1.01.130 cover (two pieces);
- B07S1.01.200 individual SPTA kit.
Version 2:
- B07S1.01.350 left-side launch module;
- B07S1.01.360 right-side launch module;
- B07S1.01.200 individual SPTA kit.
A B07S1.01.300 group SPTA kit for 30 B07S1.01.000 launchers and a set of service documentation were developed for the B07S1.01.000 launcher.
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| Right-side launch module | 9М120-1 missiles loaded on BMPT GWS |
Launcher specifications:
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Number of launcher-mounted missiles: |
4 |
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Launcher weight without package: B07S1.01.000 launcher, version 1 B07S1.01.000 launcher, version 2 |
108 kg, max. 119 kg, max. |
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Missile arrangement on launch module: B07S1.01.000 launcher, version 1 B07S1.01.000 launcher, version 2 |
stacked staggered outwards |
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Overall dimensions of launcher components: B07S1.01.000 launcher, version 1: - B07S1.01.150 left-side launch module - B07S1.01.160 right-side launch module B07S1.01.000 launcher, version 2: - B07S1.01.350 left-side launch module - B07S1.01.360 right-side launch module |
920х263х431 mm, max. 920х263х431 mm, max.
920х418х330 mm, max. 920х418х330 mm, max. |