Güdümlü Anti Tank Füzeleri(ATGM)

Güdümlü Anti Tank Füzeleri(ATGM)

AGM-114 HELLFİRE


Origin:United States Manufacturer:Lockheed Martin

Specifications:
Weight: 100–108lb (45.4–49kg) [1]
Length: 64 in (163 cm) Diameter: 7 in (17.8 cm)
Wingspan: 13 in (33 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
Engine:Solid-fuel rocket  

Operational
range:500 m – 8 km

Speed: Mach 1.3 (950 mph; 425 m/s)

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

MİLAN

Origin:France-
West Germany
History In service: 1972–present
Used by: 41 countries Designed :1970 Manufacturer :MBDA , Bharat Dynamics (under license)
Produced: 1972
Number built: 350,000 missiles, 10,000 launchers
Variants MILAN 1, MILAN 2, MILAN 2T, MILAN 3,
MILAN ER

Specifications:
Weight: 7.1 kg
Length: 1.2 m
Diameter: 0.125 m
Wingspan: 0.26 m

Warhead: tandem HEAT Detonation
mechanism contact
Engine: solid-fuel rocket 

Operational
range: 400–2000 m
Speed: 200 m/s

Guidance
system: SACLOS 

Launch
platform: Individual, Vehicle

SPİKE


Origin: Israel
History In service :1997 -  Used Wars: Second Intifada, 2006 Lebanon War, War in Afghanistan (2001 –present), Gaza War
Designed:1987 Manufacturer:Rafael Advanced Defense Systems
Diehl BGT Defence (Now part of Rheinmetall Defence Electronics)  Specifications: Weight
:Spike-ER from helicopter: • Missile in canister: 34 kg (74 lb 15 oz) • Launcher: 55 kg (121 lb 4 oz) • Launcher + 4 missiles: 187 kg (412 lb 4 oz) Spike-MR/LR from ground: [1] • Missile round: 14 kg (30 lb 14 oz) • Command & launch unit (CLU): 5 kg (11 lb 0 oz)
• Tripod: 2.8 kg (6 lb 3 oz) • Battery: 1 kg (2 lb 3 oz) • Thermal sight: 4 kg (8 lb 13 oz)
Length:1,670 mm (5 ft 6 in) (Missile w/ launcher) Diameter: 170 mm (6.7 in) (Missile w/launcher) Maximum range: 800 to 25,000 m depending on version Sights 10× optical sight
Warhead:Tandem-charge HEAT warhead  Engine:Solid-fuel rocket Guidance
system: Infrared homing - Electro Optical (CCD, IR or Dual CCD/IIR), Passive CCD or dual CCD/IIR seeker


Spike-SR
the short range version of the
weapon, minimum range is 200 m
(660 ft) while the maximum range is
800 m (2,600 ft) and is intended for
infantry use. The reusable Command
& launch unit (CLU), battery, tripod and the thermal sight are also used
by other land-based versions (with
the exception of Spike NLOS ) of the Spike missile family, each weighing 5
kg (11 lb 0 oz), 1 kg (2 lb 3 oz), 2.8
kg (6 lb 3 oz), and 4 kg (8 lb 13 oz) respectively.[1]

Spike-MR
the medium range version. The
weight of the missile is 14 kg (30 lb
14 oz), minimum range is 200 m
(660 ft) while the maximum range is
2,500 m (8,200 ft) and is used by infantry and special forces.[6] Spike-LR long range version. The weight of
the missile is 14 kg (30 lb 14 oz),
maximum range is 4,000 m (13,000
ft) and is used by infantry and light
combat vehicles. It adds fiber-optic
communication to and from the launching soldier during flight.[7] Reported armour penetration
capability is more than 700 mm (28
in) of Rolled homogeneous armour (RHA). [8]

Spike-ER
extended range or extra long range
version of the weapon. It was
formerly also known as the NT- Dandy or NT-D. It has a maximum range of 8,000 m (26,000 ft).[9] It has a larger diameter and is heavier
than the other systems, and is
usually vehicle mounted. It is used
by infantry, LCVs , and helicopters. The Finnish Navy's Coastal Jaegers also operates the version in the anti-
ship role. The weight of the missile is
34 kg (74 lb 15 oz), the launchers
are 30 kg (66 lb 2 oz) and 55 kg
(121 lb 4 oz) respectively for the
vehicle and air-launched versions. Penetration is around 1,000 mm (39 in)

BGM-71 TOW

Origin: United States  History In service: 1970–present
Designer: Hughes Aircraft Company Designed 1963–1968

Specifications:
Length: 1.16–1.17 m (probe folded) 1.41–1.51 m (probe extended) Diameter: 0.152 m
Wingspan 0.46 m

Warhead: weight 3.9–5.9 kg 
Operational
range: 3,750 m

Guidance
system: Optically-tracked, wire-guided

UMTAS



Origin:Turkey Manufacturer:Roketsan A.S.

Specifications:
Weight: 37.5 kg [1] Length :175 cm
Diameter: 16 cm

Warhead:
Insensitive Anti-armor Tandem
Warhead
Engine: Solid-fuel rocket

Operational
range :500 – 8000 m

Guidance
system: Imaging Infrared Seeker

Launch
platform: Rotary wing platforms
Unmanned combat air vehicles

ERYX

Origin: France
Canada
History In service:1994 Used by:Operators Designed :1985-92 Manufacturer:MBDA Produced :1993

Specifications
Weight:16.0 kg (13.0 kg missile and container, firing post 4.0 kg)
Length:0.905 m (2.97 ft) Diameter:0.136 m (5.4 in)

WARHEAD:137 mm diameter 3.6 kg tandem HEAT (penetrating 900 mm RHA behind reactive armour[1], or 2.5 m through concrete)

Operational Range: 50–600 m
Speed 18 m/s (65 km/h ) at launch to 245 m/ s (880 km/h) at 600 m

Guidance:
system SACLOS wire Launch:
platform Individual, Vehicle


http://i16.photobucket.com/albums/b24/hybenamon/LAND/MISSILES/ERYX%20-%20FRENCH%20AT%20MISSILE/eryx-7.jpg

FGM-148 JAVELİN



Origin:United States  History In service: 1996– Users Wars Operation: Enduring Freedom (2001– present) Operation Iraqi Freedom / Operation New Dawn (2003–present)
Designer: Texas Instruments and Martin Marietta (now Raytheon and Lockheed Martin ) Designed June 1989 Manufacturer: Raytheon and Lockheed Martin
Unit cost:$40,000 (£20,000) (missile); $
125,000 (reusable Command Launch
Unit)

Specifications:
Weight: Missile- 11.8 kg (26 lb) [1] 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 range: 75 to 2500 m

Warhead: Tandem shaped charge HEAT Warhead weight: 8.4 kg (18.5 lb) [2]

Engine: Solid fuel rocket

Guidance
system: Imaging infrared (IIR)

KORNET


Origin:Russia
History In service:1994-present
Designer:KBP Instrument Design:Bureau Manufacturer:KBP Instrument 
Variants: 9M123, 9M123-2, 9M123F, 9M123F-2

Specifications:
(9M133)
Weight: 27 kg (29 kg with launch tube)
Length :1200 mm Diameter :152 mm

Warhead: 1000-1200 mm RHA [1] penetration after ERA with Tandem HEAT , Thermobaric Warhead weight 7 kg HEAT, 10 kg TNT equivalent
Thermobaric

Engine: Solid-fuel rocket

Operational
range: 100-5500m

Guidance
system: SACLOS laser beam riding

RBS 56 BILL


Origin: Sweden History In service: 1985-
Used by: Sweden, Austria , Lithuania, Brazil  Manufacturer: Bofors Produced: 1985 - lte 1990s
Number built: 15,000 +

Specifications:
Weight: 36 kg (launcher) Length: 900 mm Diameter:150 mm   

Effective range: 150 to 2,200 m

LAHAT

Origin: Israel
Service: 1992 - present Used by: Israel, India
Unit cost $20,000 (1999)

Specifications
Weight: 13.5 kg
Length: 97.5 cm Diameter: 105 mm Warhead: Tandem HEAT Warhead weight: 4.5 kg Operational
range: 8000 m
Speed: 285-300 m/s

Guidance
system :Semi-Active Laser Homing
Launch
platform: 105 - 120 mm smooth bore