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Fairey Delta 2




The Fairey Delta 2 or FD2 was a British supersonic research aircraft produced in response to a specification from the Ministry Of Supply for investigation into flight and control at transonic and supersonic speeds.

The design was a mid wing delta monoplane, on a circular cross section fuselage with no tailplane. The engine was a Rolls-Royce Avon with an afterburner. The Delta 2 had a very long tapering nose which obscured forward vision during landing, take-off and movement on the ground. To compensate, the nose section and cockpit dropped 10 degrees in a similar way to that used on Concorde later. Two aircraft were built.

The first FD2 was aircraft WG774 which made its maiden flight on 6 October 1954 , under the command of Fairey test pilot Peter Twiss . In March 1956, this aircraft broke the World Air Speed Record raising it to 1132 mph (1820 km/h), an increase of some 300 mph (480 km/h) over the record set in year before by an F-100 Super Sabre , and thus became the first aircraft to exceed 1000 mph in level flight. This aircraft was later converted to become the BAC 221 for aerodynamic research for Concorde and is now on display alongside the British Concorde prototype at the Fleet Air Arm Museum at Yeovilton. The second FD.2 ( WG777 ) is preserved at the Royal Air Force Museum at RAF Cosford alongside many other supersonic research aircraft.


SPECIFICATIONS (FAIREY DELTA 2)


  plane Or Copter plane
  jet Or Prop jet
  Crew 1
  length Main 51 ft 7 in
  length Alt 157 m
  span Main 26 ft 10 in
  span Alt 82 m
  height Main 11 ft
  height Alt 34 m
  area Main 360 ft&sup2
  area Alt 33 m&sup2
  empty Weight Main 11,000 lb
  empty Weight Alt 4,990 kg
  max Takeoff Weight Main 13,884 lb
  max Takeoff Weight Alt 6,298 kg
  engine (jet) Rolls-Royce RA5
  type Of Jet Turbojet
  number Of Jets 1
  max Speed Main 1,122 mph
  max Speed Alt 2,078 km/h
  range Main 830 mi
  range Alt 1,340 km
  climb Rate Main 15,000 ft/min
  climb Rate Alt 762 m/s
  loading Main lb/ft&sup2
  loading Alt kg/m&sup2



REFERENCES

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