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<!--BEGIN SPECIFICATIONS--> F-111 Aardvark Specifications Primary Function: Multipurpose tactical fighter bomber Contractor: General Dynamics Corporation Crew: Two (pilot and weapon systems officer) Unit Cost: FY98 $75 million [Total Program] Powerplant Two Pratt & Whitney TF30-P-100 turbofans rated at 25,100 lb (11,250 kilograms) each Dimensions Length: 73 feet, 6 inches (22.0 meters) Wingspan: 63 feet (19 meters) full forward 31 feet, 11 1/2 inches (11.9 meters) full aft Height: 17 feet, 1 1/2 inches (5.13 meters) Weights Empty: 47,481 pounds (21,367 kilograms) Maximum Takeoff: 100,000 pounds (45,000 kilograms) Performance Speed: Mach 1.2 at sea level Mach 2.5 at 60,000 feet Ceiling: 60,000-plus feet (18,200 meters) Range: 3,565 miles (3,100 nautical miles) with external fuel tanks Armament Up to four nuclear bombs on four pivoting wing pylons, and two in internal weapons bay. Wing pylons carry total external load of 25,000 pounds (11,250 kilograms) of bombs, rockets, missiles, or fuel tanks <!--END SPECIFICATIONS--> <!--BEGIN ACHIEVEMENTS--> F-111 Aardvark Achievements The F-111 featured numerous notable innovations, including variable-geometry wings and a cockpit escape capsule. <!--END ACHIEVEMENTS--> <!--BEGIN FEATURES--> F-111 Aardvark Features The F-111 has variable-sweep wings that allow the pilot to fly from slow approach speeds to supersonic velocity at sea level and more than twice the speed of sound at higher altitudes. Wings angle from 16 degrees (full forward) to 72.5 degrees (full aft). The F-111 needs no drag chute or reverse thrust to slow down after landing. The two crew members sit side-by-side in a pressurized cockpit module that serves as an emergency escape vehicle and as a survival shelter on land or water. The aircraft's wings and much of the fuselage behind the crew module contain fuel tanks. Using internal fuel only, the plane has a range of more than 2,500 nautical miles. External fuel tanks can be carried on the pylons under the wings and jettisoned if necessary. Source: http://www.au.af.mil <!--END FEATURES--> <!--BEGIN BACKGROUND--> F-111 Aardvark Background The F-111 is a multipurpose tactical fighter bomber capable of supersonic speeds. It can operate from tree-top level to altitudes above 60,000 feet. The F-111 can carry conventional as well as nuclear weapons . It can carry up to two bombs or additional fuel in the internal weapons bay. External ordnance includes combinations of bombs, missiles and fuel tanks. The loads nearest the fuselage on each side pivot as the wings sweep back, keeping ordnance parallel to the fuselage. Outer pylons do not move but can be jettisoned for high-speed flight. The F-111A first flew in December 1964. The first operational aircraft was delivered in October. A models were used for tactical bombing in Southeast Asia. Developed for the U.S. Navy, the F-111B was canceled before its production. F-111C's are flown by the Royal Australian Air Force. The F-111D has improved avionics with better navigation, air-to-air weapon delivery systems, and newer turbofan engines. The E model has modified air intakes to improve the engine's performance at speeds above Mach 2.2. The F-111F has Improved turbofan engines give F-111F models 35 percent more thrust than previous F-111A and E engines. The avionics systems of the F model combine features of the F-111D and E. The last F-model was delivered to the Air Force in November 1976. The F models have been modified to carry the Pave Tack system in their weapons bays. This system provides an improved capability to acquire, track and designate ground targets at night for delivery of laser, infrared and electro-optically guided weapons. Source: http://www.au.af.mil <!--END BACKGROUND-->
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