Hobby Master HA3031 USAF General Dynamics F-111A "Aardvark" Strike Aircraft - 66-0022, "Combat Lancer", Takhli RTAB, Thailand, 1968 (1:72 Scale)
"Tell the Vietnamese they've got to draw in their horns or we're going to bomb them back into the Stone Age. And we would shove them back into the Stone Age with Air power or Naval power, not with ground forces."
- General Curtis LeMay, May 1964
The General Dynamics F-111 "Aardvark" is a medium-range interdictor and tactical strike aircraft that also fills the roles of strategic bomber, reconnaissance, and electronic warfare in its various versions. Developed in the 1960s and first entering service in 1967, the United States Air Force (USAF) variants were officially retired by 1998. The Royal Australian Air Force (RAAF) is the sole remaining operator of the F-111.
The F-111 pioneered several technologies for production military aircraft including variable-sweep wings, afterburning turbofan engines, and automated terrain following radar for low-level, high-speed flight. Its design was influential, being reflected in later Soviet aircraft such as the Sukhoi Su-24, and some of its advanced features have since become commonplace. During its inception, however, the F-111 suffered a variety of development problems, and several of its intended roles, such as naval interception through the F-111B, failed to materialize.
In USAF service the F-111 has been effectively replaced by the F-15E Strike Eagle for medium-range precision strike missions, while the supersonic bomber role has been assumed by the B-1B Lancer. In 2007, the RAAF decided to replace its 21 F-111s in 2010 with 24 F/A-18F Super Hornets.
Pictured here is a 1:72 scale replica of a RAAF General Dynamics F-111C "Aardvark" strike aircraft that was known as the "Combat Lancer", then deployed to Takhli RTAB, Thailand, during 1968.
Sold Out!
Dimensions:
Wingspan: 12-1/4-inches
Length: 10-1/2-inches
Release Date: October 2023
Historical Account: "Combat Lancer" - In the fall of 1967, PACAF began deployment planning for its first General Dynamics F-111As, the initial Air Force version of the TFX (for "Tactical Fighter Experimental"), the most controversial of all of the McNamara era's joint-service "commonality" airplanes, intended as "cost effective" alternatives to aircraft procured via traditional acquisition processes.
The F-4, OV-10, and A-7 programs demonstrated that if properly conceived and executed, commonality could work, but, as told by Richard P. Hallon in his book Rolling Thunder 1965-68, with the TFX, McNamara had attempted the impossible - building a successful airplane by merging inherently contradictory requirements: a Navy requirement for a long-loiter fleet air defense fighter with a large and powerful radar and new long-range missiles; an Air Force requirement for a supersonic-dash nuclear and conventional strike aircraft; and the Kennedy administration's requirement that the resulting design also be capable of operating off austere airfields, reflecting its fixation on counterinsurgency (COIN).
Key to meeting all these was a large variable-geometry wing that fully extended to generate the lift necessary to achieve long-range and long-loiter, but swept sharply back to reduce drag, permitting supersonic dash. In 1963, Congressional investigators found that the McNamara team had rejected the recommendations of service and NASA professionals when it selected General Dynamics over a more highly regarded Boeing design.
Once in flight testing the TFX revealed serious performance and safety deficiencies, many requiring redesign. The F-111B carrier-based variant, greatly overweight and dangerously under-powered, never entered fleet service, forcing the Navy to develop a substitute, the Grumman F-14A Tomcat, which first flew over a dozen years after the F-4 had taken to the air.
- General characteristics
- 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
- Bombs:
- Free-fall general-purpose bombs
- Mk 82 (500 lb/227 kg)
- Mk 83 (1,000 lb/454 kg)
- Mk 84 (2,000 lb/907 kg)
- Mk 117 (750 lb/340 kg)
- Cluster bombs
- BLU-109 (2,000 lb/907 kg) hardened penetration bomb
- Paveway laser-guided bombs, including:
- GBU-10 (2,000 lb/907 kg)
- GBU-12 (500 lb/227 kg)
- GBU-28, specialized 4,800 lb (2,200 kg) penetration bomb
- BLU-107 Durandal runway-cratering bomb
- GBU-15 electro-optical bomb
- AGM-130 stand-off bomb
Wingspan: 12-1/4-inches Length: 10-1/2-inches
|