Vickers VC10

Vickers VC10
Страны	Великобритании
Роль	Узкофюзилный реактивный авиалайнер и воздушный топливозаправщик
Первый полет	9 июня 1962
Построен	54

Vickers VC10 — британский реактивный авиалайнер среднеразмерного размера, узкофюзный дальнемагнитосерный реактивный авиалайнер, спроектированный и построенный компанией Vickers-Armstrongs (Aircraft) Ltd и впервые поднявшийся в воздух в Бруклендсе, графство Суррей, в 1962 году. Авиалайнер был разработан для работы на дальних маршрутах с более коротких взлетно-посадочных полос той эпохи и отличался отличной горячей и высокой производительностью для операций из африканских аэропортов.

Источник: Vickers VC10 в Википедии

Vickers VC10 Walk Around
Фотограф	Говард Мейсон
Локализации	Неизвестная
Фотографии	65

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General Characteristics and Role

The Vickers VC10 was a long-range, narrow-body jet airliner designed and built by Vickers-Armstrongs (later British Aircraft Corporation) in the United Kingdom. It was specifically engineered for hot and high environments, featuring oversized wings and powerful, rear-mounted engines that gave it exceptional takeoff performance from challenging airfields, particularly in Africa and Asia. Although fewer were built than its competitor, the Boeing 707, the VC10 was famous for its speed, quiet cabin, and elegant design, earning it the title of “The Queen of the Skies” among many pilots and passengers. It saw extensive service with British Overseas Airways Corporation (BOAC) and later had a long and distinguished second career with the Royal Air Force (RAF) as a transport and aerial refueling tanker (VC10 K versions).

Property	Typical Value (VC10 Type 1101/K3 Tanker)
Роль	Long-Range Airliner, Military Transport/Tanker
National Origin	Великобритания
Производителя	Vickers-Armstrongs / BAC
First Flight	29 June 1962
Экипажа	4 (Pilot, Co-pilot, Flight Engineer, Navigator)
Capacity (Airliner)	135 – 151 passengers
Длина	48.36 m (158 ft 8 in)
Размах крыла	44.55 m (146 ft 2 in)
Высота	12.04 m (39 ft 6 in)
Empty Weight	66,500 kg (146,600 lb)
Max Takeoff Weight	146,500 kg (323,000 lb)

Powerplant and Performance

Engines: 4 x Rolls-Royce Conway Mk. 540 turbofan engines.
Thrust (Each): 91.9 kN (20,700 lbf).
Engine Configuration: Uniquely featured four engines mounted in pairs on the sides of the rear fuselage, minimizing wing bending and noise in the passenger cabin.
Maximum Speed: Mach 0.86 (933 km/h; 580 mph).
Cruise Speed: Mach 0.82 (886 km/h; 550 mph).
Range (Typical): 9,415 km (5,850 mi; 5,084 nmi).
Service Ceiling: 13,100 m (43,000 ft).

Variants and Retirement

Standard VC10: Initial production model.
Super VC10: Stretched fuselage version with a greater range and capacity (up to 151 passengers).
VC10 K2/K3/K4: Military conversion of former civilian airliners into aerial refueling tankers for the RAF.
Retirement: The VC10 had an exceptionally long service life; the last remaining airframes, operated by the RAF as tankers, were retired in 2013, over 50 years after the first flight.
Legacy: It was the fastest jet airliner in operation between the UK and New York until the introduction of the Concorde.