Modern Tank killer

saat ini senjata anti tank sudah berupa Anti Tank guided missile (ATGM), yaitu misil terpadu yang fungsi utamanya adalah menghancurkan tank lapis baja dan kendaraan tempur lapis baja lainya. berikut ini adalah beberapa jenis  ATGM :

FGM-148 Javelin
U.S. Army soldiers firing an FGM-148 Javelin.
Type	Anti-tank guided missile launcher
Place of origin	United States
Service history
In service	1996–present
Used by	See Users
Wars	Operation Enduring Freedom (2001–present) Operation Iraqi Freedom (2003–present)
Production history
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)
Produced	1996–present
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]
Detonation mechanism	Impact force
Engine	Solid fuel rocket
Guidance system	Imaging infrared (IIR)

MILAN
MILAN 1 missile
Type	Anti-tank
Place of origin	France  Germany
Service history
In service	1972–present
Used by	41 countries
Production history
Designed	1970s
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
Warhead	tandem HEAT
Detonation mechanism	contact
Engine	solid-fuel rocket
Wingspan	0.26 m
Operational range	400–2000 m
Flight ceiling	-
Speed	200 m/s
Guidance system	SACLOS wire
Steering system	Thrust Vector
Launch platform	Individual, Vehicle

ERYX
ERYX missile, in launch tube, loaded on firing post
Type	Anti-tank
Place of origin	France  Canada
Service history
In service	1994
Used by	Operators
Production history
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 0.9 m through 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

Spike
SPIKE ATGM Command & launcher unit (CLU) with mock-up SPIKE LR missile mounted on a tripod at Singapore Army Open House 2007
Type	Man-portable fire-and-forget anti-tank missile
Place of origin	Israel
Service history
In service	1997 - Present
Used by	See Operators
Wars	Second Intifada, 2006 Lebanon War, War in Afghanistan (2001–present), Gaza War
Production history
Designed	1987
Manufacturer	Rafael Advanced Defense Systems Diehl BGT Defence (Now part of Rheinmetall Defence Electronics)
Produced	1997 - Present
Variants	See Versions
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)
Rate of fire	Ready to launch in 30 seconds, reload in 15 seconds
Maximum range	800 to 25,000 m (2,600 to 82,000 ft) depending on version
Sights	10× optical sight
Warhead	Tandem-charge HEAT warhead
Detonation mechanism	Impact
Engine	Solid-fuel rocket
Guidance system	Infrared homing - Electro Optical (CCD, IR or Dual CCD/IIR), Passive CCD or dual CCD/IIR seeker

AGM-114 Hellfire
A model of a Hellfire's components
Type	Air-to-surface and surface-to-surface missile
Place of origin	United States
Production history
Manufacturer	Lockheed Martin
Specifications
Weight	100–108lb (45.4–49kg)[1]
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 (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

9M133 Kornet
9M133 missile with launcher
Type	Anti-tank missile
Place of origin	Russia
Service history
In service	1994-present
Used by	See users
Production history
Designer	KBP Instrument Design Bureau
Manufacturer	KBP Instrument Design Bureau
Variants	9M123, 9M123-2, 9M123F, 9M123F-2
Specifications (9M133)
Weight	27 kg (29 kg with launch tube)
Length	1200 mm
Diameter	152 mm
Warhead	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	100-5500m
Guidance system	SACLOS laser beam riding
Steering system	Two control surfaces
Accuracy	<5 m