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SH-60 Seahawk
 
       
    General Characteristics:
Primary Function: Varies with the particular military service.
Contractor: Sikorsky Aircraft Corporation (airframe); General Electric Company (engines); IBM Corporation (avionics components).
Propulsion: Two General Electric T700-GE-700 or T700-GE-701C engines; thrust: up to 1,940 shaft horsepower.
Length: 64 feet 10 inches (19.6 meters).
Height: Varies with the version; from 13 to 17 feet (3.9 to 5.1 meters).
Rotor Diameter: 53 feet 8 inches (16.4 meters).
Weight: Varies; 21,000 to 23,000 pounds (9,450 to 10,350 kg).
Airspeed: 180 knots maximum.
Range: Generally about 380 nautical miles (600 km); range becomes unlimited with air refueling capability.
Crew: Three to four.
 
       

SH-60 Seahawk

SH-60 Seahawk