Handley Page HP.115

Handley Page HP.115
Страны	Великобритании
Роль	Экспериментальные самолеты
Первый полет	17 августа 1961 года
Построен	1

Teh Страница Хюмли HP.115 был британский дельта крыло научно-исследовательский самолет, построенный Хингли Пейдж для проверки низкой скорости обработки характеристик можно ожидать от сверхзвукового авиалайнера стройной конфигурации дельты. Она в рамках британской программы исследований сверхзвуковых самолетов, осуществленной в 1960-х годах и спонсируемой министерством снабжения, которая в конечном итоге произвела Concorde.

Источник: Страница Хюди HP.115 в Википедии

HP.115 Walk Around
Photographer	Howard Mason
Localisation	Fleet Air Arm Museum
Photos	23

Л.С.115 1

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Л.С.115 9

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Handley Page HP.115 (Prototype) Walk Around
Фотограф	Unknow
Локализации	Неизвестная
Фотографии	21

Страница Хюмли HP.115

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General Characteristics and Role

The Handley Page HP.115 was a small, experimental British research aircraft built to investigate the flight characteristics of an extremely slender delta wing at low speeds. It was part of a major research program in the United Kingdom aimed at developing the supersonic transport—the eventual Concorde. The HP.115’s specific purpose was to determine the handling qualities and low-speed stability needed for landing the proposed supersonic airliner. The aircraft had a fixed tricycle undercarriage and a high-mounted engine. Only one prototype was ever built (serial number XP841). Although limited in speed and range, the HP.115 successfully completed its research objectives, logging nearly 400 flights before being retired.

Property	Typical Value (HP.115)
Роль	Experimental Research Aircraft
National Origin	Великобритания
Производителя	Handley Page Aircraft Company
First Flight	17 августа 1961 года
Экипажа	1 (Pilot)
Длина	15.47 m (50 ft 9 in)
Размах крыла	6.60 m (21 ft 8 in)
Wing Area	37.2 m² (400 sq ft)
Empty Weight	2,240 kg (4,940 lb)
Max Takeoff Weight	3,450 kg (7,600 lb)

Powerplant and Performance

Engine: 1 x Bristol Siddeley Viper 9 turbojet engine.
Thrust: 8.41 kN (1,890 lbf).
Wing Sweep: Extremely slender delta wing with a 74.7° leading-edge sweep, which was the key experimental feature.
Maximum Speed: Approx. 399 km/h (248 mph; 215 kn).
Service Ceiling: 5,000 m (16,400 ft).
Crucial Contribution: The flight data collected from the HP.115 was vital in confirming the stability and control characteristics that would be incorporated into the Concorde’s design.

Status and Legacy

Testing Period: The HP.115 carried out research flights at the Royal Aircraft Establishment (RAE) Bedford between 1961 and 1974.
Retirement: The sole prototype was retired from flying in 1974.
Preservation: The single Handley Page HP.115 is now preserved and on public display at the Fleet Air Arm Museum at RNAS Yeovilton, Somerset, UK.