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MH-60G Pave Hawk
 
       
    General Characteristics
Primary Function:
combat search and rescue and military operations other than war in day, night or marginal weather conditions.
Contractor: United Technologies/Sikorsky Aircraft Company
Power Plant: Two General Electric T700-GE-700 or T700-GE-701C engines
Thrust: 1,560-1,940 shaft horsepower, each engine
Rotor Diameter: 53 feet, 7 inches (14.1 meters)
Length: 64 feet, 8 inches (17.1 meters)
Height: 16 feet, 8 inches (4.4 meters)
Weight: 22,000 pounds (9,900 kilograms)
Maximum Takeoff Weight: 22,000 pounds (9,900 kilograms)
Fuel Capacity: 4,500 pounds (2,041 kilograms)
Payload: depends upon mission
Speed: 184 mph (159 knots)
Range: 504 nautical miles
Ceiling: 14,000 feet (4,267 meters)
Armament: Two 7.62mm or .50 caliber machineguns
Crew: Two pilots, one flight engineer and one gunner
Unit Cost: $9.3 million (fiscal 1998 constant dollars)
Initial operating capability: 1982
Inventory: Active force, 64; ANG, 18; Reserve, 23
 
       

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk

MH-60G Pave Hawk