Vickers V-1000
Vickers V-1000
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Vickers V-1000

The Vickers-Armstrongs V-1000 was a proposed jet-powered cargo aircraft that was designed to meet a requirement issued by the British Ministry of Supply which sought a strategic transport for the Royal Air Force (RAF) to support its strategic bomber fleet, particularly the V-bombers. The design bears many similarities to the Vickers Valiant, one of the V-bombers, but also featured substantial changes. In addition to its military application, both the Ministry and Vickers also intended to use the same basic design as the VC7, a six-abreast trans-Atlantic jet airliner for British Overseas Airways Corporation (BOAC).

In 1955, by which point the prototype was already largely complete, the Ministry of Supply decided to terminate the V-1000 project in mid-development. By that time, the design had garnered interest from airlines, and had led to re-designs being conducted by competing US manufacturers, influencing the design of the Boeing 707 and Douglas DC-8. The V-1000 has been called one of the great "what-ifs" of British aviation, and its cancellation was the topic of considerable debate in the House of Commons.

We have handed to the Americans, without a struggle, the entire world market for big jet airliners.

— George Edwards, Vickers managing director,

During the early 1950s, Britain's civil aircraft industry was releasing and manufacturing a number of competitive and innovative aircraft designs. They include the de Havilland Comet, the world's first jet-powered commercial transport aircraft, the Vickers Viscount, the world's first turboprop-powered commercial airliner, and the Bristol Britannia, a turboprop-powered aircraft capable of conducting routine transatlantic flights. All of those designs had their origins in the specifications laid out by the wartime Brabazon Committee. With those aircraft, Britain appeared to be on track to capturing a large slice of the global demand for civil aircraft for the foreseeable future.

Meanwhile, the Royal Air Force (RAF) had been pursuing development of a new generation of strategic bombers: the Vickers Valiant, the Avro Vulcan, and the Handley Page Victor. Armed with nuclear weapons and powered by jet engines, those aircraft would be entering service during the 1950s as the V-bombers. The first of the V-bombers to enter service was the Valiant. Noting the favourable performance attributes of the Valiant, both the Ministry of Supply (MoS) and Vickers became interested in a prospective transport derivative, as a potential long-range successor to the smaller Comet. The RAF had also noticed a demand for a suitable transport aircraft capable of accompanying the V-bombers on deployments to any part of the world, carrying a mix of personnel and cargo needed for such deployments, while having similar speed and range capabilities to the bomber force.

Vickers received a request from the MoS for submissions of the Valiant transport derivative. At the same time, the British Overseas Airways Corporation (BOAC) was also interested in a potential commercial airliner from Vickers; thus, the company was naturally excited that it would be possible to develop an aircraft that would serve as both a military transport, being procured for the RAF, and as a commercial airliner, that BOAC would be expected to order. Such a move would mean increased financial support for the program as well as improved access to development and testing resources. According to aviation author Derek Wood, Sir George Edwards, who headed the design, viewed the military variant "as a stepping stone to the civil version", which was internally designated as the VC7.

Working in direct cooperation with BOAC throughout the studies performed for the project, Vickers came to quickly recognise that producing a suitable aircraft would not be a straightforward matter of simply pairing the Valiant's wings onto a new fuselage suitable for transport duties. Amongst the changes required would be an entirely new structure, the adoption of roomy and pressurised cabin, and more powerful engines. RAF requirements also provided some complications for the design, such as necessitating the use of double-slotted flaps to achieve the short field performance sought, along with the integration of a rear-mounted sizable hydraulic freight elevator for self-loading operations. Crucially, it was recognised that, in order for the aircraft to be economically viable against competing aircraft powered by turboprop engines and traditional piston engines, an engine capable of more thrust and superior specific fuel consumption than the Valiant's Rolls-Royce Avon turbojet engine would be necessary.

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