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  • General Dynamics / Grumman EF-111 Raven Electronic Warfare Aircraft (EWA)

    The Grumman EF-111 Raven was a direct EWA conversion of the F-111A Aardvark fighter-bomber strike platform.

     Updated: 6/18/2017; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com

    The EF-111 Raven was developed from a United States Air Force need for an Electronic Warfare Aircraft (EWA) to replace its aging fleet of EB-66 platforms. The EF-111 was born directly from the airframe of the existing F-111 Aardvark series of swing-wing bomber aircraft already in service and extended the operational use of the airframe by decades. With a single unit conversion cost of $25 million on top of the already paid $15 million production cost, the EF-111 became an expensive yet important addition to USAF operations during the latet years of the Cold War. The system would see operational service up until the late 1990's to which then the Air Force was forced to rely on US Navy and Marine Corps aircraft to fulfill the same EWA role. In any case, the EF-111 platform proved to be versatile and reliable and performed well under the stresses of combat.

    By 1972 the United States Air Force was already showcasing its F-111 swing-wing bombers throughout the skies over Vietnam. Seeing the potential for replacing the EB-66 conversion models, the USAF tabbed some F-111A models to be converted themselves into the EF-111, taking on the designation name of "Raven" in the process. These new systems would adopt state-of-the-art technologies to help other aerial battlefield components fight more effectively and accurately. Grumman proceeded on the conversion plans under a new USAF contract in 1974 with first flight achieved by a Raven in 1977. Deliveries would start four years later.

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    General Dynamics / Grumman EF-111A Raven Technical Specifications

    Service Year: 1981
    Type: Electronic Warfare Aircraft (EWA)
    National Origin: United States
    Manufacturer(s): General Dynamics / Grumman - USA
    Production Total: 42

    Structural (Crew Space, Dimensions and Weights)

    Operating Crew: 2
    Length: 76.02 feet (23.17 meters)
    Width: 62.99 feet (19.20 meters)
    Height: 20.01 feet (6.10 meters)

    Weight (Empty): 55,274 lb (25,072 kg)
    Weight (MTOW): 89,001 lb (40,370 kg)

    Installed Power and Standard Day Performance

    Engine(s): 2 x Pratt & Whitney TF30-P-3 (later TF30-P-9) turbofan engines with afterburner developing 20,840 lb of thrust each.

    Maximum Speed: 1,855 mph (2,985 kph; 1,612 knots)
    Maximum Range: 2,000 miles (3,218 km)
    Service Ceiling: 44,997 feet (13,715 meters; 8.52 miles)
    Rate-of-Climb: 11,000 feet-per-minute (3,353 m/min)

    Armament / Mission Payload

    2 x AIM-9 Sidewinder air-to-air missile
    2 x 600 gallon external fuel tanks

    Global Operators / Customers

    United States (retired)

    Model Variants (Including Prototypes)

    F-111A - Production Model on which the EF-111A is based on.

    EF-111A - Single Series Conversion Models of F-111A models for electronic warfare role.