page_title: Fairey Delta 2
section_title: Specifications (Fairey Delta 2)
hierarchical_section_title: Fairey Delta 2 / Specifications (Fairey Delta 2)
caption_attribution_description: Fairy Delta 23
context_page_description: The Fairey Delta 2 or FD2 was a British supersonic research aircraft produced by the Fairey Aviation Company in response to a specification from the Ministry of Supply for a specialised aircraft for conducting investigations into flight and control at transonic and supersonic speeds. Features included a delta wing and a drooped nose. On 6 October 1954, the Delta 2 made its maiden flight, flown by Fairey test pilot Peter Twiss; two aircraft would be produced. The Delta 2 was the final aircraft to be produced by Fairey as an independent manufacturer.
  The Fairey Delta 2 was the first jet aircraft to exceed 1000 mph in level flight. On 10 March 1956, it set a new world speed record of 1,132 mph. The Delta 2 held the absolute World Air Speed Record for over a year. It continued to be used for flight testing, and was allocated to the Royal Aircraft Establishment in 1958.
  A testbed aircraft was required to verify design calculations and wind tunnel results for the Concorde "ogee delta" wing design so one of the aircraft was extensively rebuilt as the BAC 221. On 1 May 1964, the modified aircraft performed its first flight.
context_section_description: General characteristics
  Crew: 1
  Length: 51 ft 7.5 in (15.74 m)
  Wingspan: 26 ft 10 in (8.18 m)
  Height: 11 ft 0 in (3.35 m)
  Wing area: 360 sq ft (33.44 m²)
  Empty weight: 11,000 lb (4,990 kg)
  Gross weight: 13,884 lb (6,298 kg)
  Powerplant: 1 × Rolls-Royce Avon 200 , 10,000 lbf (44 kN) thrust
  Performance
  Maximum speed: 1,300 mph (2,092 km/h, 1,100 kn)
  Range: 830 mi (1,336 km, 720 nmi)
caption: Close-up rear view of the Delta 2
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