The General Dynamics F111 is not a jet fighter, but a striker aircraft. We like this military plane for various reasons. Firstly because it pioneered various technologies such as the variable sweep wings that has then been implemented on many fighter jets, but also for its “rise of the phoenix” story. The F111 was developed in the early 60s by GD. The first prototype flew in December 1964 and from the start, the aircraft appeared as ill-conceived for its duties. Ordered for the Navy, it was too big, too heavy to fit on an aircraft carrier. Its avionics were approximate and the plane suffered from severe drag. The first operational use of the F111 during the Vietnam War was a disaster as it suffered many losses.

Not at its best in flight, the F111 is still a reference for the technologies it pioneered. The sweep wings, afterburning turbofan engines, automated following terrain radar for automated low level flight at very high speed. The F111 is fast, Mach 2.5 and is a long range aircraft. Despite all its assets, it failed to exercise its duties until redevelopments were done in the 1970s. Its rise of the phoenix started in 1972 during Operation Linebacker in Southeast Asia taking place in very bad weather conditions. The F111 was the only aircraft taking off and did not need refueling to accomplish its mission. In April 1986, 18 F111 were used during operation El Dorado Canyon, to strike Libya. Taking off from Britain, the jet strikers flew all the way to northern Africa, dropped their loads and returned. And it was during Desert Storm that the F111 was estimated 47% more capable than all other striker aircrafts engaged in the conflict.
Two countries have used the F111. The USA and Australia. The US Airforce have retired the F111 in 1998, replaced by various jet fighters: the F15E Strike Eagle for medium range precision strike missions and the B1B Lancer for its role as a supersonic bomber. Australia will decommission its fleet of F111 in December 2010. The official farewell ceremony will be held on the 2nd and 3rd December at Amberely. The good news is for all jet fighter rides enthusiasts that they plan to let people in to say goodbye and one lucky guy will have the chance to get in the back seat for a final flight. Cost has yet to be given, but we will let you know as soon we do.
The F111 specifications
Crew: 2 (pilot and weapons system operator)
Length: 73 ft 6 in (22.4 m)
Wingspan:
Spread: 63 ft (19.2 m)
Swept: 32 ft (9.75 m)
Height: 17.13 ft (5.22 m)
Wing area:
Spread: 657.4 ft² (61.07 m²)
Swept: 525 ft² (48.77 m²)
Airfoil: NACA 64-210.68 root, NACA 64-209.80 tip
Empty weight: 47,200 lb (21,400 kg)
Loaded weight: 82,800 lb (37,600 kg)
Max takeoff weight: 100,000 lb (45,300 kg)
Powerplant: 2× Pratt & Whitney TF30-P-100 turbofans
Dry thrust: 17,900 lbf (79.6 kN) each
Thrust with afterburner: 25,100 lbf (112 kN) each
Zero-lift drag coefficient: 0.0186
Drag area: 9.36 ft² (0.87 m²)
Aspect ratio: spread: 7.56, swept: 1.95
Performance
Maximum speed: Mach 2.5 (1,650 mph, 2,655 km/h)
Combat radius: 1,330 mi (1,160 nmi, 2,140 km)
Ferry range: 4,200 mi (3,700 nmi, 6,760 km)
Service ceiling: 66,000 ft (20,100 m)
Rate of climb: 25,890 ft/min (131.5 m/s)
Wing loading:
Spread: 126.0 lb/ft² (615.2 kg/m²)
Swept: 158 lb/ft² (771 kg/m²)
Thrust/weight: 0.61
Lift-to-drag ratio: 15.8
Armament
Guns: 1× M61 Vulcan 20 mm (0.787 in) gatling cannon (seldom fitted)
Hardpoints: 9 in total (8× under-wing, 1× under-fuselage between engines)
Armament capacity: 31,500 lb (14,300 kg) ordnance mounted externally on hardpoints and internally in fuselage weapons bay
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