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EA-6B Prowler
 
       
    General Characteristics:
Primary Function:
Electronic countermeasures.
Contractor: Northrop Grumman Systems Corporation.
Date Deployed: First Flight: 25 May 1968
Operational Capability: July 1971.
Propulsion: Two Pratt & Whitney J52-P408 engines (10,400 pounds thrust each).
Length: 59 feet 10 inches (17.7 meters).
Height: 16 feet 8 inches (4.9 meters).
Wingspan: 53 feet (15.9 meters).
Weight: Maximum Take Off Gross Weight: 61,500 pounds (27,450 kg).
Airspeed: 500 Kts + (575 mph, 920 kmh).
Ceiling: 37,600 feet.
Range: 1,000 nautical miles+ (1,150 miles, 1,840 km).
Crew: Pilot and three electronic countermeasures officers.
Armament and Avionics:
AGM-88 HARM antiradar missiles.
ALQ-99 Tactical Jamming System (TJS) external pods.
USQ-113 communications jamming system.
 
       

 

EA-6B Prowler

EA-6B Prowler

EA-6B Prowler

EA-6B Prowler

EA-6B Prowler