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Hunting H.126

Supersonic and Experimental Aircraft

The Hunting H.126 was a British experimental aircraft designed and built by Hunting Aircraft to test the jet flap, a blown-flap system that routes engine exhaust over the wing flaps to cut take-off and landing speeds. The Ministry of Aviation issued Specification ER.189D, and Hunting won a contract in 1959 to build two aircraft. Only one, serial XN714, was completed. It was a shoulder-wing monoplane with a T-tail, powered by a single Bristol Orpheus turbojet whose exhaust fed sixteen wing nozzles and control nozzles in the tail and wing tips. It flew on 26 March 1963 and made about 100 test flights for the Royal Aircraft Establishment until 1967, was tested by NASA in 1969, was withdrawn in 1972 and is now displayed at the Royal Air Force Museum Cosford.

Facts
Year
1963 1
Engine Class
Jet 1
Status
Retired from service 1
Units Built
1 1
Mass (kg)
3738 1
Maximum Mass (kg)
4872 1
Engine
Bristol Siddeley BOr.3 Orpheus Mk.805 turbojet engine 1
Comparison
Body Style
Aircraft (no road body style) 1
Connections

Exemplifies

Aviation, Modes
Source Hunting H.126 (Wikipedia)

Of Make

Source Hunting H.126 (Wikipedia)
In the Other Atlases

Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Hunting H.126 (Wikipedia)Lead, maker
Quote, Lead, maker
designed and built by British aviation company Hunting Aircraft

Originated In

Also in Geography Atlas: where this subject originated.

Source Hunting H.126 (Wikipedia)Lead, origin
Quote, Lead, origin
designed and built by British aviation company Hunting Aircraft
Sources
1. Hunting H.126 (Wikipedia)
  • Lead, maiden flight
    This aircraft performed its maiden flight on 26 March 1963.
  • Lead
    The Hunting H.126 is an experimental aircraft
  • Design, powerplant
    The H.126 was powered by a single Bristol Orpheus turbojet engine.
  • Specifications, powerplant
    Bristol Siddeley BOr.3 Orpheus Mk.805 turbojet engine, 4,000 lbf (18 kN) thrust
  • Specifications, empty weight
    Empty weight: 8,240 lb (3,738 kg)
  • Specifications, maximum take-off weight
    Max takeoff weight: 10,740 lb (4,872 kg)
  • Lead, units built
    Only the single aircraft was ever completed
  • Lead, withdrawal
    the aircraft was officially withdrawn in 1972
  • Lead, maker
    designed and built by British aviation company Hunting Aircraft
  • Lead, origin
    designed and built by British aviation company Hunting Aircraft
  • In Group: Experimental Jet Research Aircraft, Lead, kind of craft
    The Hunting H.126 is an experimental aircraft
  • Exemplifies: Aviation, Lead, kind of craft (mode)
    The Hunting H.126 is an experimental aircraft
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