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UH-60 Blackhawk



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The Black Hawk is the Army's most important utility helicopter used for air assault, air cavalry, and aeromedical evacuation units. It can carry 11 combat-loaded, air assault troops, the Black Hawk also has a cargo hook and it can lift a 105-millimeter field howitzer and 30 rounds of ammunition, or a terrian vehicle like the Humvee.
The helicopter can be configured to carry out medical evacuation, command-and-control, search-and-rescue, armed escort, electronic warfare and executive transport missions.

The Blackhawk was first deployed in 1978, the Black Hawk's advanced technology makes it easy to maintain in the field. The UH-60A, was developed for troop transport, command and control, MedEvac, and reconnaissance, to replace the UH-1 Series "Huey" in the combat assault role.
Both the pilot and co-pilot are provided with armor-protective seats. Protective armor on the Black Hawk can withstand hits from 23mm shells.
The Black Hawk has a composite titanium and fiberglass four-bladed main rotor, is powered by two General Electric T700-GE-700 1622 shp turboshaft engines, and has a speed of 163 mph (142 knots).

Specifications

Manufacturer: Sikorsky Aircraft
Main rotor diameter: 53 ft 8 inches
Tail rotor diameter: 11 ft 0 inches
Maximum height to top turning tail rotor: 16ft 9 inches
Width fuselage: 7 ft 9 inches
Empty weight: 11,780 lbs
Mission gross weight: 16,864 lbs
Maximum gross weight: 22,000 Ibs
Engines: Two General Electric T700-GE-701 C
Power: 1,940 shaft horsepower
Internal fuel: 360 US gallons (1,360 litres)
External auxiliary fuel tanks: 460 US gallons (1740 litres)
Endurance on internal fuel: 3 hours 5 minutes
Maximum endurance with auxiliary fuel: 7 hours 21 minutes
Performance at 16,864 lbs Missions Gross Weight:
Maximum Cruise Speed at 5,000 ft: 162 kts
Service ceiling: 19,000 ft

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