General Dynamics · United States · ICAO: F111 · 1967–1976 ·
$10.3 million (1973)

The General Dynamics F-111 Aardvark is developed by General Dynamics in the 1960s as a medium-range interdictor and tactical attack aircraft. The aircraft is also suitable for strategic nuclear bombing, aerial reconnaissance, and as well as electronic warfare. In 1967, the F-111 Aardvark entered service with the United States Air Force. In 1973, it also entered service with the Royal Australian Air Force.

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Engine:
2× Pratt & Whitney TF30-P-100
Engine type:
Turbofan
Thrust:
2 × 25,100 lbf  ·  112 kN
Avionics:
GMR and TFR
Wing Tips:
No winglets
Seats:
2
Exterior length:
73 ft 6 in · 22.40 m
Tail height:
17 ft 2 in · 5.22 m
Fuselage diameter:
ft 3 in · 1.60 m
Wing span / rotor:
62 ft 12 in · 19.20 m
Max takeoff weight:
100,000 lb  ·  45,400 kg
Max Payload:
31,500 lb  ·  14,300 kg
Fuel capacity:
5,000 gal  ·  19,000 L  ·  15,200 kg  (Jet A)
Max cruise speed:
1,434 kt  ·  1,650 mph  ·  2,656 km/h
Range:
3,210 nm  ·  3,690 mi  ·  5,940 km
Ceiling:
66,000 ft  ·  20,100 m
Rate of climb:
25,890 ft/min  ·  132 m/s
Takeoff distance:
3,300 ft  ·  1,000 m
Landing distance:
3,950 ft  ·  1,200 m

Blog Mentions

Blog posts that mention the General Dynamics F-111 Aardvark:

The 18 Fastest Fighter Jets in The World

The “Cadillac of the F-111 force” and the last version produced for Tactical Air Command was designated as the F-111F. In 1969, the United States Air Force accepted the development of the version. It was produced from 1970 to 1976 with a total number of 106 F-111Fs built. It has an external length of 22.40 meters, an external height of 2.7 meters, and a fuselage width of 1.6 meters. The strengthened wing has a wingspan of 19 meters, a lower swept wingspan of 9.8 meters, and a wing area of 61.07 square meters when spread and 48.8 square meters when swept. It has a tail height of 5.22 meters and a wheelbase of 7.3 meters. The aircraft has an empty weight of 21,410 kg ad a gross weight of 37,557 kg. The maximum takeoff weight is 45,359 kg and the maximum payload is 14,300 kg. It has a fuel tank capacity of 5,020 US gal.

The F-111F is powered by two Pratt and Whitney TF30-P-100 afterburning turbofan engines. It is a low-bypass turbofan which produces a maximum dry thrust of 17,900 lbf each and 25,100 lbf with afterburner. The maximum speed is 1,434 knots at altitude and 795 knots at sea level. It has a ferry range of 3,210 nautical miles with external drop tanks. The aircraft can fly up to 66,000 feet and can climb at a rate of 25,890 feet per minute.

The F-111F version could be loaded with a single 20 mm M61A1 Vulcan six-barreled Gatling cannon in the bomb bay. It has nine hardpoints; eight under the wings and one under the fuselage, plus two attach points in the bomb bay with a capacity of 14,300 kg with provisions to carry combinations of AGM-69 SRAM thermonuclear air-to-surface missile and various bombs such as AGM-130 stand-off bomb, free-fall general-purpose bombs, cluster bombs, hardened penetration bomb, paveway laser-guided bombs, runway-cratering bomb, electro-optical bomb, and nuclear bombs.

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