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.

Country of Origin:United States
Manufacturer:General Dynamics - USA
Initial Year of Service:1967
Production:554

Focus Model:General Dynamics F-111F Aardvark
Crew:2

Length:73.49ft (22.4m)
Width:62.99ft (19.20m)
Height:17.13ft (5.22m)
Weight (Empty):47,179lbs (21,400kg)
Weight (MTOW):100,002lbs (45,360kg)

Powerplant:2 x Pratt & Whitney TF30-P-111 turbofan engines generating 25,100lbs of standard thrust each.

Maximum Speed:1,650mph (2,655kmh; 1,434kts)
Maximum Range:4,200miles (6,760km)
Service Ceiling:65,945ft (20,100m; 12.5miles)
Rate-of-Climb:25,890 feet per minute (7,891m/min)

Hardpoints:5
Armament Suite:
OPTIONAL:
1 x 20mm M61 Vulcan cannon