General Dynamics F-111K
|Artist's impression of F-111K|
|National origin||United States|
|Primary user||Royal Air Force (intended)|
|Number built||50 (intended)|
|Program cost||£280 million (1966)|
|Developed from||General Dynamics F-111 Aardvark|
|Serial||XV884 - XV887
XV902 - XV947
The General Dynamics F-111K was a planned variant of the General Dynamics F-111 Aardvark medium-range interdictor and tactical strike aircraft by General Dynamics, to meet a requirement for such an aircraft for the Royal Air Force.
The project was initiated in 1965 following the cancellation of the BAC TSR-2 strike aircraft. The aircraft was planned as a hybrid of several variants of the F-111 as a way of producing an aircraft for the specific needs of the United Kingdom. A RAF order for 50 aircraft, made in 1967, was cancelled a year later.
In the early 1960s, the British Aircraft Corporation was in the process of developing a new strike aircraft for the Royal Air Force to replace the English Electric Canberra. This aircraft, designated as "TSR-2" (Tactical Strike and Reconnaissance), had a large set of requirements listed by the government, and had led to TSR-2 becoming a hugely complex machine; it was intended that it be able to undertake both conventional and nuclear strike missions at high and low level, in all weathers, at supersonic speeds. As a consequence, the costs of the project began to increase, leading to it becoming the most expensive aviation project in British history, at a time when defence spending was being cut. This led to the RAF being asked to look for potential alternatives to TSR-2, in the event of it being cancelled.
At the same time, the Royal Australian Air Force were also looking for a Canberra replacement, and were looking at a number of options, including both TSR-2 and the General Dynamics F-111 then being developed for the USAF's TFX programme. The uncertainty over TSR-2 led to the Australians selecting an adapted version of the F-111 in 1963. The RAF were asked to evaluate the F-111 as a cheaper option for the strike aircraft requirement, although the incoming Labour government denied it planned to cancel the British aircraft. This denial was reversed in April 1965, when TSR-2 was cancelled and a decision taken to look into the option of acquiring up to 110 F-111s instead.
No firm commitment was made to the F-111 until the publication of the 1966 Defence White Paper, although it was the government's preferred option. Following the publication of the defence review, it was announced that up to 50 F-111s would be procured for the RAF; like the Australian version, these would be highly adapted to suit the unique set of British requirements. The intention was to form an initial four operational squadrons, plus an OCU, with two stationed in the UK and two forming part of the UK's forces East of Suez. The intention was that long-range, land based F-111s would be used to replace the strike capability of the CVA-01 aircraft carriers that were cancelled in the White Paper. Although there was no public announcement as to specific squadrons that would receive the F-111, a document from early 1966 by the AOC-in-C of Bomber Command, Air Chief Marshal Sir Wallace Kyle, indicated that 12 Squadron (then a Vulcan squadron assigned to the strategic nuclear role), together with the inactive 7, 15 and 40 Squadrons, would receive the aircraft upon their delivery.
In April 1966, a firm order was placed for 10 F-111s for the RAF, with options for another 40, covering the standard F-111K models and a number of dual-control TF-111K trainers, with the purchase price set around £2.1m ($5.95m) per unit (1965 prices). This was intended to show a significant reduction in cost when compared with the development and estimated production costs of TSR-2. At the same time, a pair of Victor squadrons had been moved out of RAF Honington, which was earmarked for conversion to accommodate the F-111 force. However, at the same time the actual cost of F-111 production had increased; in April 1967, when the RAF's 40 additional aircraft were ordered, the per unit cost of the F-111C for the Royal Australian Air Force was US$9m. This eventually led to an admission from the British government that the cost would increase from the initial figure set out – in 1967, the then Secretary of State for Defence, Denis Healey, stated that adjusting for inflation was taken into account, which would add approximately 2.5% to the cost of each aircraft. This did not include the cost of installing the British adaptations. The total estimate cost by the time the last aircraft was due to be delivered in 1970 was approximately £2.7m. Despite this, the government still maintained that the F-111 programme (combined with the proposed AFVG) would be cheaper than TSR-2 to the tune of approximately £700m.
The first two aircraft began assembly in July 1967, and were issued with the serial numbers XV884 and XV885. These were intended as development aircraft, to undertake airframe, avionics and weapons testing prior to them being refurbished as operational units. At the same time, the remainder of the planned 50 strong fleet were allocated serials from XV886-887 (TF-111K) and XV902-947 (F-111K). The first two airframes were in the final stages of assembly at General Dynamics' plant at Fort Worth, Texas in early 1968 when the Government then issued a new policy that would see the majority of British forces stationed East of Suez withdrawn by 1971. At the same time it also decided to cancel the F-111K procurement. The devaluation of sterling in 1967 had led to the per unit cost rising to approximately £3m. Additionally, the production schedules were slipping; while the RAAF had its first F-111 delivered in 1968, official acceptance of the type into service did not occur until 1973 due to structural and development problems (which led to the RAAF having to lease 24 F-4 Phantoms as an interim measure). All of the components that had been assembled for the production of the main F-111K fleet that shared commonality were diverted to the FB-111A program, while the two aircraft under construction were re-designated as YF-111As with the intention that they be used as test aircraft in the F-111A program. Ultimately however, the two F-111Ks were never operated as test aircraft – in July 1968, almost exactly a year after the first airframe began construction, the US Air Force decided not to take them over, and General Dynamics were ordered to use them for component recovery.
The cancellation of the F-111K still left a requirement for a strike aircraft to replace the Canberra, so the government ordered 26 new Blackburn Buccaneer aircraft for the RAF to operate alongside ex-Fleet Air Arm Buccaneers that were being moved to the air force following the phased withdrawal of fixed wing carrier aviation in the Royal Navy – somewhat ironically, the Buccaneer had been rejected as a contender for the original RAF requirement that had led first to the selection and cancellation of TSR-2, and subsequently the F-111K. No. 12 Squadron, one of the units that had been proposed to operate the F-111, became operational as the first RAF Buccaneer squadron at Honington in 1969. With responsibility for the UK's nuclear deterrent passing to the Royal Navy in 1969, Avro Vulcans were transferred from the strategic bomber role to the long range air interdiction role that would have been fulfilled by the F-111.
The ending of the F-111 procurement, combined with the cancellation of the Anglo-French Variable Geometry project, led to Britain eventually joining the multi-national working group to develop the "Multi-Role Combat Aircraft" in 1968; this led to the formation of Panavia and the ultimate development of the Tornado, an aircraft that assumed the roles of low-level strike and long range interdiction planned for the F-111.
The F-111K was to be based around the airframe of the original F-111A version built for the U.S. Air Force, but was to feature a number of alterations and adaptations. Structurally, the aircraft would be similar to F-111A with the heavy duty undercarriage from the strategic bomber version. This allowed for a greater gross weight to be designed into the aircraft. The other major design change from the F-111A was in its avionics, with the design calling for the Mark II package developed for the F-111D version, which featured a new inertial navigation and attack system, incorporating the Rockwell International AN/APQ-130 attack radar, an IBM on-board computer, the Marconi AN/APN-189 doppler navigation radar and the Sperry Corporation AN/APQ-128 terrain following radar. The plan was then to pair this avionics package with British designed and developed mission systems, of which the main elements were the reconnaissance capability and weapon carriage. The F-111K was to feature a revised weapons bay, containing a new removable centreline weapons pylon, which was beneficial given the design of the underwing pylons – the F-111 had four stations under each wing, but only the inner pair were designed to pivot, meaning that the outer pair could not be used with the wings in full sweepback mode. All of the weapon pylons featured British designed ejector rack units. The aircraft was given provision for a pallet inside the weapons bay that would feature a British designed reconnaissance system, with three camera windows located next to the nosewheel undercarriage (which the US versions were not fitted with). The aircraft was designed with an aerial refuelling probe compatible with the "probe and drogue" system used by the RAF, similar to the one fitted to the F-111B, although mounted differently.
Data from Wilson and Pittaway
- Crew: 2 (pilot and weapons system operator)
- Length: 22.4 m (73.0 ft)
- Spread: 19.2 m (63.0 ft)
- Swept: 9.75 m (32 ft) (34.0 ft)
- Height: 5.22 mm (17.1 ft)
- Wing area:
- Spread: 657.4 ft² (61.07 m²)
- Swept: 525 ft² (48.77 m²)
- Powerplant: 2 × Pratt & Whitney TF30-P-100 turbofans
- Maximum speed: Mach 2.5
- Hardpoints: 9 in total (8 × under-wing, 1 × underfuselage in weapons bay)
- Rockwell AN/APQ-130 attack radar
- Sperry AN/APQ-128 J-Band terrain following radar
- Marconi AN/APN-189 Doppler navigation radar
- Related development
- General Dynamics F-111 Aardvark
- General Dynamics/Grumman F-111B
- General Dynamics/Grumman EF-111A Raven
- General Dynamics F-111C
- Aircraft of comparable role, configuration and era
- Related lists
- "UK Military Aircraft Serial Allocations: XV". UK Serials Resource Centre. Retrieved 7 June 2013.
- Conclusions of a Meeting of the Cabinet held at 10 Downing Street, S.W.1, on Thursday, 1st April, 1965, at 10 p.m., CC(65)21, CAB/128/39. London: Public Record Office, 2010.
- Hunter, Alexander (1998). TSR2 with Hindsight (PDF). Brighton: RAF Historical Society. p. 39. ISBN 0-9519824-8-6. Retrieved 31 May 2013.
- Healey, D. W. The Need for an Option on the F-111A, C(65)58, CAB/129/121. London: Public Record Office, 2010.
- "F-111K on the eve of the deadline". Flight International. Royal Aero Club. 91 (3029): 480–481. 1967. Retrieved 16 May 2013.
- Cooper, Sir Frank (1993). "The Direction of Air Force Policy in the 1950s and 1960s" (PDF). Proceedings of the Royal Air Force Historical Society. Royal Air Force Historical Society (11): 19. Retrieved 30 May 2013.[permanent dead link]
- "What if the F 111K had entered RAF service as planned?". 21 May 2008. Retrieved 29 May 2013.
- "RAF Honington Station History". RAF Honington. Royal Air Force. Retrieved 29 May 2013.
- "F-111K cost increases". Flight International. Royal Aero Club. 91 (3032): 616. 1967. Retrieved 14 May 2013.
- "Mr Healey's missing £700 million". Flight International. Royal Aero Club. 91 (3037): 831–832. 1967. Retrieved 16 May 2013.
- Logan 1998, p. 279
- Logan 1998, p. 278
- Gardner 1981, p. 116.
- Baugher, Joe (8 May 2000). "General Dynamics F-111C". joebaugher.com. Retrieved 16 May 2013.
- "More Buccaneers – and more cuts". Flight International. Royal Aero Club. 94 (3097): 113–114. 1968. Retrieved 16 May 2013.
- "About the Vulcan". avrovulcan.com. Vulcan Restoration Trust. Retrieved 30 May 2013.
- Baugher, Joe (17 January 2005). "General Dynamics F-111D". joebaugher.com. Retrieved 16 May 2013.
- Wilson and Pittaway 2010, p. 8.
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