Anti-tank Missiles - ATGMs

[BLACKEAGLE]

United Kingdom

Swingfire

Type Anti-tank missile
Place of origin United Kingdom
Service history
Used by See text
Production history
Produced 1966-1993
Number built 46,650
Specifications
Weight 27 kg
Length 1.07 m
Diameter 0.17 m
Warhead 7 kg HEAT

Detonation mechanism
Impact
Engine Solid rocket motor
Wingspan 0.39 m

Operational
range
150 - 4,000 m
Flight ceiling n/a
Speed 185 m/s

Guidance system
Wire, MCLOS/SACLOS

Steering system
Thrust Vector Control

Launch platform
Vehicle


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Brimstone (missile)

Type Air-to-surface missile
Place of origin United Kingdom
Service history
In service 2005
Used by Royal Air Force
Royal Saudi Air Force
Wars Operation Telic
Operation Herrick
Operation Ellamy
Operation Shader
Production history
Designer GEC-Marconi
Designed 1996
Manufacturer MBDA (UK) Ltd, Lostock
Unit cost (Dual Mode Variant)
£105,000/unit[1]
£175,000 inc development
Produced 1999
Variants Single mode
Dual Mode Sensor
Brimstone 2
Sea Spear
Specifications
Weight 48.5 kg
Length 1.8 m
Diameter 17.8 cm
Warhead HEAT tandem warhead

Detonation mechanism
Crush (impact) fuze
Engine Solid-fuel rocket

Operational range

Brimstone I:
20+ km (12+ mi) from fixed wing, 12 km (7.5 mi) from rotor wing

Brimstone II:
60+ km (37+ mi) from fixed wing, 40+ km (25+ mi) from rotor wing
Speed Supersonic (~450m/s)

Guidance system
94 GHz millimetric wave Active radar homing and INS autopilot, dual-mode adds laser guidance
Accuracy = sub-1m CEP

Steering system
Flight control surfaces

Launch platform
Tornado GR4
Typhoon (planned)
Ship (planned)

 

[BLACKEAGLE]

United States

M47 Dragon

Type Anti-tank missile
Place of origin United States
Service history
In service 1975–2001
Used by See Operators
Wars Iran-Iraq War, Gulf War
Production history
Designer Raytheon
Designed March 3, 1966
Manufacturer McDonnell Douglas, Raytheon
Unit cost $13,000 (standard)
$51,000 (with night tracking system)
Produced 1975
Number built 7,000 launchers, 33,000 missiles (U.S. Army)
17,000 missiles (U.S. Marine Corps)
Variants Dragon II, Super Dragon, Saeghe 1 and 2
Specifications (FGM-77)
Length 1,154 mm (45.4 in)
Diameter 140 mm
Crew 1
Effective firing range 1,000 meters, minimum 75 meters
Maximum firing range 1,000–1,500 meters
Warhead Hollow charge
Speed 200 m/s (660 ft/s)

Guidance system
SACLOS system sights


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FGM-148 Javelin

Type Anti-tank missile
Place of origin United States
Service history
In service 1996–present
Used by See Operators
Wars Operation Enduring Freedom (2001–present)
Operation Iraqi Freedom / Operation New Dawn (20 March 2003 – 15 December 2011)
Production history
Designer Texas Instruments and Martin Marietta
(now Raytheon and Lockheed Martin)
Designed June 1989
Manufacturer Raytheon and Lockheed Martin
Unit cost US$246,000(FY2014) (FGM-148F)
Produced 1996–present
Number built 40,000
Specifications
Weight 22.3 kg (49.2 lb) (carry weight)
Detachable CLU: 6.4 kg (14.1 lb)
Length Missile: 1.1 m (43 in)
Launch tube: 1.2 m (47 in)
Diameter Missile: 127 mm (5.0 in)
Launch tube: 142 mm (5.6 in)
Crew 2
Effective firing range 75 to 2500 m
Maximum firing range 4,750 m (tested)
Warhead Tandem shaped charge HEAT
Warhead weight 8.4 kg (18.5 lb)

Detonation mechanism
Impact force
Engine Solid fuel rocket

Guidance system
infrared homing

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FGM-172 SRAW

Type Anti-Tank Missile Launcher
Place of origin United States
Service history
In service 2002–present
Used by United States
Production history
Designer Lockheed Martin
Designed 2002
Manufacturer Lockheed Martin
Produced 2003–present
Specifications
Weight 9.7 kg (21 lb)
Length 70.5 cm (2 ft 33⁄4 in)
Width 14 cm (5.5 in)
Cartridge Single Shot
Caliber 139.7mm. (Fires 139mm. Rockets)
Muzzle velocity 900 km/h (560 mph)
Effective firing range 17 to 600 m (19 to 660 yd)
Filling EFP - Explosively Formed Penetrator (original version, now replaced with multipurpose blast warhead)

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BGM-71 TOW

Type Anti-tank missile
Place of origin United States
Service history
In service 1970–present
Used by See Operators
Production history
Designer Hughes Aircraft Company
Designed 1963–1968
Specifications
Length 1.16–1.17 m (probe folded) 1.41–1.51 m (probe extended)
Diameter 152mm
Warhead weight 3.9–6.14 kg
Wingspan 0.46 m

Operational range
up to 4,200 m
Speed 278–320 m/s

Guidance system
Optically tracked, Wire-guided missile

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AGM-114 Hellfire

Type Air-to-surface and surface-to-surface missile
Place of origin United States
Service history
In service 1984–present
Production history
Manufacturer Lockheed Martin
Unit cost US$110,000
Produced 1974–present
Specifications
Weight 100–108 lb (45.4–49 kg)
Length 64 in (163 cm)
Diameter 7 in (17.8 cm)
Warhead High Explosive Anti-Tank (HEAT); 20 lb (9 kg) tandem anti-armor
Metal augmented charge (MAC); 18 lb (8 kg) shaped-charge
Blast Fragmentation
Engine Solid-fuel rocket
Wingspan 13 in (33 cm)

Operational range
546 yd – 5 mi (500 m – 8 km)
Speed Mach 1.3 (995 mph; 450 m/s; 1591 km/h)

Guidance system
Semi-active laser homing
millimeter wave radar seeker

Launch platform
Rotary- and fixed-wing platforms, Unmanned combat air vehicles, tripods, ships, and ground vehicles

 

[BLACKEAGLE]

Russia

9K121 Vikhr

Type air-launched anti-tank missile
Place of origin Russia
Service history
In service 1985 – present
Used by Russian Air Force
Production history
Manufacturer KBP Instrument Design Bureau
Unit cost Unknown
Produced 1985 – present
Specifications
Weight 45 kg
Length 2.80 m
Diameter 130 mm
Warhead 8-12 kg tandem HEAT charge, armor penetration behind ERA, 1,000 mm

Detonation mechanism
Proximity and Impact
Engine solid-fuel rocket
Wingspan 380 mm
Propellant solid fuel

Operational range
8-10 km
Speed 600m/s, Mach 1.8

Guidance system
Laser beam riding

Launch platform

Helicopters

• Ka-50
• Ka-52

Aircraft

• Su-25T

Ships

• AK-630 Vikhr-K

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9M123 Khrizantema

Type Anti-tank missile
Place of origin Russia
Service history
In service 2005-present
Used by Russia
Wars Libyan Civil War
Production history
Designer KBM (Kolomna)
Designed 1996
Manufacturer KBM
Produced 2005-present
Variants 9M123, 9M123-2, 9M123F, 9M123F-2
Specifications (9M123)
Weight 46 kg (54 kg with launch tube)
Length 2057 mm
Diameter 150 mm
Warhead Tandem HEAT (9M123), Thermobaric (9M123F)
Warhead weight 8 kg (9M123), 6 kg (9M123F)

Detonation
mechanism
Impact fuze
Wingspan 310 mm
Propellant Solid-fuel rocket

Operational range
400-6000m
Speed 400 m/s

Guidance system
ACLOS radar beam riding , SACLOS laser beam riding

Steering system
Two control surfaces
Accuracy <5 m

Launch platform
9P157-2 tank destroyer, Mi-28 Attack helicopter

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9M133 Kornet

Type Anti-tank missile
Place of origin Russia
Service history
In service 1998–present
Used by See Operators
Wars See Combat history
Production history
Designer KBP Instrument Design Bureau
Designed 1988-1998
Manufacturer Degtyarev plant
Produced 1994–present
Number built 35 000 (2009)
Variants See Variants
Specifications (9M133)
Weight 27 kg (29 kg with launch tube)
Length 1200 mm
Diameter 152 mm
Warhead 1000-1200 (9K135), 1200 (E), 1300 (D) mm RHA penetration after ERA with Tandem HEAT, Thermobaric
Warhead weight 7 kg HEAT, 10 kg TNT equivalent Thermobaric

Detonation mechanism
Impact fuze
Wingspan 460 mm
Propellant Solid-fuel rocket

Operational range

• Kornet
  100-5,500m
• Kornet-EM
  8,000 m (anti-tank),
  10,000 m (thermobaric)

Guidance system
SACLOS laser beam riding

Steering system
Two control surfaces
Accuracy <5 m

Launch platform
Individual, vehicle

 

[BLACKEAGLE]

9K115-2 Metis-M

Type Anti-tank missile
Place of origin Russia
Service history
In service 1992–present
Used by See Operators
Production history
Manufacturer KBP Instrument Design Bureau
Produced 1992–present
Specifications
Weight 13.8 kg
Length 980 mm
Diameter 130 mm
Warhead HEAT tandem warhead, Armor penetration behind ERA 900-950 mm. Thermobaric anti-personnel/anti-material warhead is also available.
Engine solid-fuel rocket

Operational range
0.08 - 2 km
Speed 200 m/s

Guidance system
SACLOS wire-guided missile


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9M117 Bastion

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9M119

Type ATGM
Place of origin Soviet Union
Service history
In service 1980s–present
Used by Russia
China
Serbia
India
Production history
Designer Tula Machinery Design Bureau (Tula KBP)
Designed 1980s
Manufacturer Degtyarev plant
Unit cost $37,500 (2012)
Produced 1980s–present
Variants 9M119M
Specifications
Weight 16.5 / 17.2 kg
Diameter 125 mm
Warhead Tandem hollow-charge
Warhead weight 4.5 kg

Operational range
4,000 / 5,000 m
Speed Subsonic

Guidance system
Laser beam riding

Launch platform
125 mm smoothbore guns

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9M120 Ataka

Type Anti-tank guided missile
Place of origin Soviet Union
Service history
In service 1985–present
Used by See Operators
Production history
Designer KBM
Designed 1980
Manufacturer Degtyarev plant
Produced 1980s–present
Variants See Variants
Specifications (9M120 Ataka)
Weight 49.5 kg (109 lb)
Length 1,830 mm (72 in)
Diameter 130 mm (5.1 in)
Warhead HEAT Tandem warhead
Warhead weight 7.4 kg (16 lb)

Detonation mechanism
Impact
Wingspan 360 mm (14 in)

Operational range
0.4–6 km (0.25–3.73 mi)
Flight ceiling 0–4,000 m (2.5 mi)
Speed 550 m/s (1,800 ft/s) (maximum)
400 m/s (1,300 ft/s) (average)

Guidance system
Radio command link SACLOS
Accuracy 0.65–0.9 Hit probability against an MBT from a distance of 4 km.

Launch platform
Armored fighting vehicles and helicopters

 

[BLACKEAGLE]

9K112 Kobra

Type Anti-tank missile
Place of origin Soviet Union
Service history
In service 1976–present
Used by Soviet Union
Production history
Designer KB Tochmash
Designed 1970s
Produced 1975–1979 (9M112), 1979–1984 (9M112M)
Variants 9M112M, 9M112M2, 9M124
Specifications
Weight 23.2 kg
Effective firing range 100–4,000 meters
Warhead weight 4.5 kg

Guidance system
SACLOS radio

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9K115 Metis

Type Anti-tank missile
Place of origin Soviet Union
Service history
In service 1979 – present
Used by Russia
Production history
Manufacturer KBP Instrument Design Bureau
Produced 1978 – present
Variants 9K115-2 Metis-M
Specifications
Weight 5.5 kg (12 lb);
6.3 kg (14 lb) w/container
Length 740 mm (29 in)
Diameter 94 mm (4 in)
Warhead HEAT shaped charge
Warhead weight 2.5 kg (5.5 lb)
Wingspan 300 mm (12 in)

Operational range
40–1,000 m (130–3,280 ft)
Speed 223 m/s (732 ft/s)

Guidance system
Wire-guided SACLOS

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9M113 Konkurs

Type Anti-tank missile
Place of origin Soviet Union
Service history
In service 1974–present
Used by See operators
Production history
Designed 1970
Manufacturer Tula Machinery Design Bureau (Tula KBP) – Tulsky Oruzheiny Zavod
Variants 9M113M
Specifications
Weight 14.6 kg (32 lb)
Length 1,150 mm (45 in)
875 mm (34.4 in) without gas generator
Diameter 135 mm (5.3 in)
Warhead 2.7 kg (6.0 lb) 9N131 HEAT

Detonation mechanism
Contact
Engine Solid-fuel rocket
Wingspan 468 mm (18.4 in)

Operational range
70 m (230 ft) to 4 km (2.5 mi)
Flight ceiling -
Speed 200 m/s (660 ft/s)

Guidance system
Wire-guided SACLOS

Steering
system
Two control surfaces

Launch platform
Individual, vehicle

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9K111 Fagot

Type Anti-tank weapon
Place of origin Soviet Union
Service history
In service 1970 – present
Used by See Users
Wars 2008 South Ossetia war,[1] War in Donbass, Syrian civil war, Iraq War (2014–present)
Production history
Designer Tula Machinery Design Bureau (Tula KBP)
Designed 1962
Produced 1970
Variants See Models
Specifications
Weight 12.5 kg (28 lb)
Length 1,100 mm (3 ft 7 in)
Diameter 120 mm (4.7 in)
Action 400 mm versus RHA or 200 mm towards armour inclined at 60°
Rate of fire 3 rds / min
Muzzle velocity 80 m/s (180 mph; 290 km/h) at launch
186 m/s (420 mph; 670 km/h) in flight speed
Effective firing range 70–2,500 m (230–8,200 ft)
Warhead High Explosive Anti-Tank (HEAT) warhead
Warhead weight 1.7 kg High Explosive Anti-Tank (HEAT)

Guidance system
SACLOS

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9M14 Malyutka

Type Anti-tank missile
Place of origin Soviet Union
Service history
In service 1963 – present
Used by Soviet Union and others
Wars Vietnam War
Yom Kippur War
Western Sahara War
Iran–Iraq War
Gulf War
Croatian War of Independence
2006 Lebanon War
First Chechen War
Second Chechen War (by Chechen militants)
Syrian Civil War
Production history
Designer Design Bureau of Machine-Building (KBM, Kolomna)
Designed 1961-1962
Produced 1963
Variants 9M14M, 9M14P1, Malyutka-2, Malyutka-2F
Specifications
Weight 10.9 kg (9M14M)
11.4 kg (9M14P1)
12.5 kg (Malyutka-2)
~12 kg (Malyutka-2F)
Length 860 mm
1,005 mm combat ready (Malyutka-2)
Width 393 mm (wingspan)
Diameter 125 mm
Effective firing range 500–3,000 m
Warhead weight 2.6 kg (9M14M, 9M14P1)
3.5 kg (Malyutka-2, Malyutka-2F)
Speed 115 m/s (410 km/h) (9M14M, 9M14P1)
130 m/s (470 km/h) (Malyutka-2, Malyutka-2F)

Guidance system
MCLOS, SACLOS (Later variants)

 

[Khafee]

MMP​

MMP is the latest (fifth) generation land combat missile system designed for dismounted infantry as well as for integration on combat vehicles.

Featuring both fire-and-forget and man-in-the-loop operation, network-enabled MMP also receives third party target designation for indirect firing scenarios.

MMP’s design includes the growth potential necessary for a future family of missiles for modern land combat.

MMP will replace the Milan and Javelin anti-tank missiles in service with the French Army and special forces from 2017. Taking into account the battle experience gained from recent conflicts in which the French Army has been engaged, MMP is a response to the demands that have been expressed in terms of required capabilities: firing from confined spaces, “fire-and-forget”, and self-guidance with a “man-in-the-loop” facility.

CHARACTERISTICS

Weight (incl. Tube) : 15 kg

Length : 1.3 m in tactical canister

Diameter : 140 mm

Range : 4.000 m

http://www.mbda-systems.com/product/mmp/

 

[Atalay]

OMTAS Medium Range Anti-Tank Weapon System Turkey

http://www.roketsan.com.tr/en/urunl...fuzeler/omtas-orta-menzilli-anti-tank-fuzesi/

OMTAS is equipped with state of the art technologies making it e ective against all armored threats of the modern battlefield. OMTAS is a new generation, man portable middle range anti-tank weapon system, which is made up of the launching tripod, fire control unit, sighting unit (composing the launcher unit) and the missile.​

Click to see brochure.

Platforms
OMTAS was developed for use against armored targets at a range of 4 km through firing from its own tripod.
All-up-round OMTAS Missile can be integrated onto land vehicles, stabilized land platforms and remote controlled turrets.

Characteristics

• Imaging Infrared Seeker with Automatic Target Tracker
• Tandem Warhead E ective Against All Types of Heavy Armored Vehicles
• Day & Night and All Weather Operational Capabilities
• Effective Against Stationary and Moving Targets
• Lock On Before Launch / Lock on After Launch
• Fire and Forget / Fire and Update Operating Modes
• Setting Coordinates of the Target on Launcher Unit
• Firing Behind Covers
• Switching Targets
• Hit Point Update on Target
• Indoor and Outdoor Type Simulators
• Modular Design of the Launcher Unit
• Modular Design of the Launch Unit Enables Sight Unit to be Used as a Stand Alone Unit.

Technical Specifications
Range200 – 4000 mDiameter of the Missile160 mmWeight of the Missile35 kg (Inc. Launch Tube)Length of the Missile1800 mm (Inc. Launch Tube and Shock Absorbers)Weight of the Launcher Unit36 kgSeekerImaging Infrared (IIR), Uncooled TypeAttack ModesDirect and Top AttacksOperating Modes• Fire and Forget
• Fire and Update
• Lock on Before Launch
• Lock on After LaunchOperating Temperature-35°C and +60°CStorage Temperature-40°C and +60°COperating Altitude-300 m and +3000 mShelf Life of Missile10 yearsShelf Life of Launcher Unit20 yearsSight Unit on the Launcher UnitTV/Termal Camera

L-UMTAS Laser Guided Long Range Anti-Tank Missile System Turkey

http://www.roketsan.com.tr/en/urunl...gudumlu-uzun-menzilli-tanksavar-fuze-sistemi/

Products & Services

• Land Systems
• Fuze Systems
• Air Defense Systems
• Naval Systems
• Precision Guided Missiles
• Precision-Guided Munitions
• Ballistic Protection Systems
• Turn Key Facilities and Other Projects
• Test Capabilities
• 

1. 
2. 

L-UMTAS is a long range anti-tank missile system primarily developed to operate from attack helicopter platforms. L-UMTAS is equipped with state of the art technologies making it effective against all armored threats of the modern battlefield.​

Click to see brochure.

Tactical Characteristics

• Day and Night Operational Capability
• Fire Behind Mask
• Effective Against Stationary and Moving Targets
• Wide Firing Envelope Allows Off-Boresight Engagement
• Insensitive Munition Type V Capability Against Fuel Fire and Bullet Impact
• Qualified and integrated to T-129 Atak Helicopter in 2016. first serial production batch is delivered to Turkish Armed Forces in 2017

L-UMTAS can be integrated to various platforms such as helicopter, light armored vehicle, close air support aircraft, UAV, fixed ground platforms and naval platforms.

System Specifications
MISSILE
Effective Range500 m – 8000 mDiameter160 mmLength1800 mmWeight37.5 kgSeekerSemi Active LaserWarheadTandem High Energy Antitank Warhead / High Explosive Blast Fragmentation Warhead
LAUNCHER
Number of Missiles4Weight60 kgStandard InterfaceMIL-STD-1760

 

[Super Tucano]

How much is the system unit cost if Kornet and HJ10 ?