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  • General Dynamics F-111 Aardvark Long Range Strategic Medium Bomber / Tactical Strike Aircraft

    The General Dynamics F-111 Aardvark swing-wing bomber was retired in 1996 from active service with the United States Air Force followed shortly by its counterpart - the EF-111 Raven.

     Updated: 5/5/2017; Authored By Staff Writer; Content ¬©www.MilitaryFactory.com

    The General Dynamics F-111 "Aardvark" was purposely-designed as a variable geometry "swing wing" platform from the outset. The variable swing-wing philosophy would allow the aircraft to utilize three pre-determined geometric wing positions that could be called upon to change the flight characteristics of the aircraft "on the fly". The first position, with wings fully extended, was to be used when the increased weight of the aircraft - due to ordnance and/or fuel - could produce additional drag properties under the wing, assisting the aircraft on take-off. The secondary position could be utilized to attain stability and speed at high subsonic speeds. The third position, with wings completely swept back against the fuselage, could be utilized for maximum "fast-dash" performance at altitude.

    The F-111 was based on this design principle, becoming the world's first operational variable geometry swing wing aircraft - leading the way for future global counterparts in the form of the Grumman F-14 Tomcat interceptor, the Panavia Tornado multirole aircraft, the Mikoyan-Gurevich MiG-23 and MiG-27 "Flogger" strike fighters and the Sukhoi Su-17 "Fitter" bombers. Additionally, larger (and more complex) forms of the swing-wing philosophy would also arise from the developments of the Rockwell B-1 "Lancer", the Tupolev Tu-22 "Backfire" and the Tupolev Tu-160 "Blackjack" bombers.

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    General Dynamics F-111F Aardvark Technical Specifications

    Service Year: 1967
    Type: Long Range Strategic Medium Bomber / Tactical Strike Aircraft
    National Origin: United States
    Manufacturer(s): General Dynamics - USA
    Production Total: 554

    Structural (Crew Space, Dimensions and Weights)

    Operating Crew: 2
    Length: 73.49 feet (22.4 meters)
    Width: 62.99 feet (19.20 meters)
    Height: 17.13 feet (5.22 meters)

    Weight (Empty): 47,179 lb (21,400 kg)
    Weight (MTOW): 100,002 lb (45,360 kg)

    Installed Power and Standard Day Performance

    Engine(s): 2 x Pratt & Whitney TF30-P-111 turbofan engines developing 25,100 lb of standard thrust each.

    Maximum Speed: 1,650 mph (2,655 kph; 1,434 knots)
    Maximum Range: 4,200 miles (6,760 km)
    Service Ceiling: 65,945 feet (20,100 meters; 12.49 miles)
    Rate-of-Climb: 25,890 feet-per-minute (7,891 m/min)

    Armament / Mission Payload

    1 x 20mm M61 Vulcan internal cannon

    Mission-specific ordnance can include any of the following:

    GBU-12 laser-guided bomb
    GBU-10 laser guided bomb
    AGM-84 HARM anti-radar anti-radiation Missile
    AGM-142 air-to-surface missile
    AIM-9 Sidewinder air-to-air missile
    Conventional Iron / Dumb / Drop Bombs

    Global Operators / Customers

    Australia; United States

    Model Variants (Including Prototypes)

    F-111A - Initial Production Model Designation; 23 pre-production models produced; Total of 158 at production end fitted with 18,500lb TF30-P-3 powerplants; 42 converted to EF-111A Ravens.

    F-111B - Cancelled Fleet Defense Variant of which 5 pre-production models were produced.

    F-111C - Australian Export Models of which 24 were produced.

    F-111D - 96 Production Models fitted with TF30-P-0 powerplants generating 19,600lbs of thrust each.

    F-111E - 94 Production Models of this type; developed as an interim to the F-111D model.

    F-111F - 106 Production Models of this type fitted with TF30-P-111 capable of 25,100lbs of thrust each.

    F-111G - Converted FB-111A Models for European Theater use; RAAF usage of this model as well.

    F-111K - Proposed British export model with British equipment; order eventually cancelled.

    FB-111A - Strategic Bomber Model Designation; 76 examples produced; fitted with 2 x additional hardpoints, increased wingspan and TF30-P-7 powerplants generating 20,150lbs of thrust; improved electronics.

    EF-111A "Raven" - Electronic Warfare Conversion Models of F-111A series; 42 converted in this way; last to be retired from USAF use in 1998.