M1 Abrams
The M1 Abrams is an American third-generation main
battle tank produced by the United States. It is named after General Creighton
Abrams, former Army Chief of Staff and Commander of U.S. military forces in the
Vietnam War from 1968 to 1972. Highly mobile, designed for modern armored
ground warfare,[10] the M1 is well armed and heavily armored. Notable features
include the use of a powerful gas turbine engine (multifuel capable, usually
fueled with JP8 jet fuel), the adoption of sophisticated composite armor, and
separate ammunition storage in a blow-out compartment for crew safety. Weighing
nearly 68 short tons (almost 62 metric tons), it is one of the heaviest main
battle tanks in service.
The M1 Abrams entered U.S. service in 1980, replacing the M60 tank.[11] It served for over a decade alongside the improved M60A3, which had entered service in 1978. The M1 remains the principal main battle tank of the United States Army and Marine Corps, and the armies of Egypt, Kuwait, Saudi Arabia, Australia, and Iraq.
Three main versions of the M1 Abrams have been deployed, the M1, M1A1, and M1A2, incorporating improved armament, protection and electronics. These improvements, as well as periodic upgrades to older tanks, have allowed this long-serving vehicle to remain in front-line service. The M1A3 was under early development as of 2009
Production history
Designer Chrysler Defense (now General Dynamics Land Systems)
Designed 1972 – 1979
Manufacturer Lima Army Tank Plant (since 1980)
Detroit Arsenal Tank Plant (1982–1996)
Unit cost US$6.21 million (M1A2 / FY99) Estimated in 2012 as US$8.58 million (with inflation adjustment)
Produced 1979 – present
Number built 10,000+
Specifications
Weight 67.6 short tons (60.4 long tons; 61.3 t)
Length Gun forward: 32.04 ft (9.77 m)
Hull length: 26.02 ft (7.93 m)
Width 12 ft (3.66 m)
Height 8 ft (2.44 m)
Crew 4 (commander, gunner, loader, driver)
Main armament 105 mm L52 M68 rifled cannon (M1)
120 mm L44 M256 smoothbore cannon (M1A1, M1A2, M1A2SEP) with 42 rounds
Secondary armament 1 × .50-caliber (12.7 mm) M2HB heavy machine gun with 900 rounds
2 × 7.62 mm (.308 in) M240 machine guns with 8,800 rounds (1 pintle-mounted, 1 coaxial)
Engine Honeywell AGT1500C multi-fuel turbine engine
1,500 shp (1,120 kW)
Power/weight 24.5 hp/t (18.27 kW/t)
Transmission Allison DDA X-1100-3B
Suspension Torsion bar
Ground clearance 0.48 m (1 ft 7 in) (M1, M1A1)
0.43 m (1 ft 5 in) (M1A2)
Fuel capacity 500 US gallons (1,900 l; 420 imp gal)
Operational range M1A2: 426 km (265 mi)
Speed M1A2: Road 42 mph (67 km/h) (governed)
Off-road: 25 mph (40 km/h)
The M1 Abrams entered U.S. service in 1980, replacing the M60 tank.[11] It served for over a decade alongside the improved M60A3, which had entered service in 1978. The M1 remains the principal main battle tank of the United States Army and Marine Corps, and the armies of Egypt, Kuwait, Saudi Arabia, Australia, and Iraq.
Three main versions of the M1 Abrams have been deployed, the M1, M1A1, and M1A2, incorporating improved armament, protection and electronics. These improvements, as well as periodic upgrades to older tanks, have allowed this long-serving vehicle to remain in front-line service. The M1A3 was under early development as of 2009
Production history
Designer Chrysler Defense (now General Dynamics Land Systems)
Designed 1972 – 1979
Manufacturer Lima Army Tank Plant (since 1980)
Detroit Arsenal Tank Plant (1982–1996)
Unit cost US$6.21 million (M1A2 / FY99) Estimated in 2012 as US$8.58 million (with inflation adjustment)
Produced 1979 – present
Number built 10,000+
Specifications
Weight 67.6 short tons (60.4 long tons; 61.3 t)
Length Gun forward: 32.04 ft (9.77 m)
Hull length: 26.02 ft (7.93 m)
Width 12 ft (3.66 m)
Height 8 ft (2.44 m)
Crew 4 (commander, gunner, loader, driver)
Main armament 105 mm L52 M68 rifled cannon (M1)
120 mm L44 M256 smoothbore cannon (M1A1, M1A2, M1A2SEP) with 42 rounds
Secondary armament 1 × .50-caliber (12.7 mm) M2HB heavy machine gun with 900 rounds
2 × 7.62 mm (.308 in) M240 machine guns with 8,800 rounds (1 pintle-mounted, 1 coaxial)
Engine Honeywell AGT1500C multi-fuel turbine engine
1,500 shp (1,120 kW)
Power/weight 24.5 hp/t (18.27 kW/t)
Transmission Allison DDA X-1100-3B
Suspension Torsion bar
Ground clearance 0.48 m (1 ft 7 in) (M1, M1A1)
0.43 m (1 ft 5 in) (M1A2)
Fuel capacity 500 US gallons (1,900 l; 420 imp gal)
Operational range M1A2: 426 km (265 mi)
Speed M1A2: Road 42 mph (67 km/h) (governed)
Off-road: 25 mph (40 km/h)
Комментариев нет:
Отправить комментарий