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UH-60 Black Hawk

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Sikorsky UH-60 Black Hawk
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UH-60 Black Hawk helicopter.
Type Utility helicopter
Manufacturer Sikorsky Aircraft Corporation
Primary user United States Army
Unit cost US$5.9 million
Developed from Sikorsky S-70
Variants SH-60 Seahawk
HH-60 Pave Hawk
HH-60 Jayhawk

The Sikorsky UH-60 Black Hawk is a twin-turbine engine, single rotor, semi-monocoque fuselage, rotary wing helicopter. The Sikorsky S-70 medium-lift utility or assault helicopter was the winner of a United States Army competition in the late 1970s to replace the UH-1 Huey family. Though the two final competing designs were both developed to Army specifications, the UH-60 was selected over an entry from Boeing-Vertol. It would go on to serve as the basis for variants in service with other branches of the US military.

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[edit] Overview

It can perform a wide array of missions, including the tactical transport of troops, electronic warfare, and aeromedical evacuation: several Black Hawks are even used to transport the President of the United States as Marine One. In air assault operations it can move a squad of 11 combat troops with equipment or reposition the 105 mm M102 howitzer with thirty rounds of 105 mm ammunition, and a six-man crew in a single lift. Alternatively, it can carry 2,600 lb (1,170 kg) of cargo or sling load 9,000 lb (4,050 kg) of cargo. The Black Hawk is equipped with advanced avionics and electronics for increased survivability and capability, such as the Global Positioning System.

[edit] History

Image:CSA-2005-05-05-102937.jpg The Black Hawk was developed to meet a US Army requirement for a UH-1 Iroquois replacement in 1972. Three prototypes were constructed, the first (YUH-60) flying in October 1974, and evaluated against a rival (YUH-61) Boeing-Vertol design. The Black Hawk was selected for production and the UH-60A entered service with the US Army in 1979. In the late 1980s the model was upgraded to the UH-60L (First production aircraft 89-26179) which featured more power and lift with the upgrade to the -701C model of the GE engines. A newer model is being engineered (UH-60M), which will extend the service life of both UH-60A's and UH-60L's well into the 2020s, features still more power and lift and state of the art electronic instrumentation, flight controls and aircraft navigation control.

[edit] Variants

The standard UH-60 comes in many variants, and many different modifications. The standard US Army version can be fitted with wings that allow it to carry up to four external fuel tanks for extended range operations, while variants may have different capabilities and their respective equipment in order to fulfill different roles.

The unit cost varies with the version due to the varying specifications and equipment. For example, the unit cost of the Army's UH-60L Black Hawk is $5.9 million while the unit cost of the Air Force MH-60G Pave Hawk is $10.2 million.

[edit] Problems

When firing the M134 minigun, all voice communications in the cabin and outgoing radio communications are greatly impaired due to the noise generated by the weapon and crew have to resort to hand signals, which diverts their attention away from the environment outside. (This is not a design flaw in the aircraft.)[verification needed]

The UH-60M is also equipped with a new seat design that is a step backwards from the normal Lima and Alpha series crew seats, plus the crew chief seat belt system is nothing more than a perplexing spiderweb, compared to the simple crewchief seat found in a UH-60L/A.[citation needed]

[edit] Specifications (UH-60 Black Hawk)

General characteristics<h3>
  • Crew: Minimum 2 pilots
  • Capacity: 2,645 lb of cargo internally, including 14 troops or 6 stretchers, or 8,000 lb (UH-60A) or 9,000 lb (UH-60L) of cargo externally
  • Length: 64 ft 10 in (19.76 m)
  • Rotor diameter: 53 ft 8 in (16.36 m)
  • Height: 16 ft 10 in (5.13 m)
  • Disc area: 2,260 ft² (210 m²)
  • Empty weight: 10,624 lb (4,819 kg)
  • Loaded weight: 16,260 lb (7,375 kg)
  • Max takeoff weight: 24,500 lb (11,113 kg)
  • Powerplant:General Electric T700-700 free-turbine turboshafts, 1,560 hp (1,160 kW) each
<h3>Performance<h3>
  • Maximum speed: 222 mph (193 knots, 357 km/h)
  • Combat radius: 368 mi (420 nm, 592 km)
  • Ferry range: 1,380 mi (1,200 nm, 2,220 km)
  • Service ceiling: 19,000 ft (5,790 m)
  • Rate of climb: 700 ft/min (3.6 m/s)
  • Disc loading: 7.19 lb/ft² (35.4 kg/m²)
  • Power/mass: 0.959 hp/lb (158 W/kg)
<h3>Armament<h3> (The Army is now replacing the M60 machine gun with the M240.)
  • Can be equipped with VOLCANO minefield dispersal system.


[edit] Operators

Sikorsky offered the design in the defense market, leading to its purchase by over 20 other countries. It is in service with the armies of Argentina, Australia, Austria, Bahrain, Brazil, Brunei, the People's Republic of China, Colombia, Chile, Egypt, Israel, Japan, Jordan, Malaysia, Mexico, Morocco, the Philippines, Saudi Arabia, South Korea, Spanish Navy, Republic of China (Taiwan), Thailand, and Turkey. The largest and most well known user remains the United States.

[edit] References

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[edit] External links

[edit] Related content

Related development<h3>

<h3>Designation sequence<h3>

<h3>Related lists<h3>

<h3>See also<h3>

de:Sikorsky UH-60

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