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 |
0 komentar:
Posting Komentar