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Rolls-Royce Spey

Aircraft Engines

The Rolls-Royce Spey is a low-bypass turbofan engine designed and built by Rolls-Royce that entered service in 1964, powering both the BAC One-Eleven and the Hawker Siddeley Trident. It was meant for the smaller end of the civil jet airliner market and was derived from the cancelled RB.141 Medway, using the same two-spool compressor arrangement as the larger Conway with a smaller fan that gave a bypass ratio of about 0.64 to 1. A militarised version, the RB.168, re-engined the Blackburn Buccaneer and went on to power the British Phantom FG1 and FGR2 and the Nimrod, while a version co-developed with Allison became the TF41 of the LTV A-7 Corsair II. The Spey also led to the Marine Spey shipboard turbine and, with a much larger fan, to the Tay. Spey-powered airliners stayed in widespread service until the 1980s, when noise limits at European airports forced them out, and the engine has accumulated over 50 million flight hours.

Facts
Year
1964 1
Connections

Of Make

Source Rolls-Royce Spey (Wikipedia)
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Manufactured By

Also in Business Atlas: the manufacturer of this subject.

Source Rolls-Royce Spey (Wikipedia)Lead, maker
Quote, Lead, maker
originally designed and manufactured by Rolls-Royce
Sources
1. Rolls-Royce Spey (Wikipedia)
  • Lead
    since its introduction in 1964
  • Lead, maker
    originally designed and manufactured by Rolls-Royce
  • In Group: Turbojet and Turbofan Engines, Lead, engine type
    is a low-bypass turbofan engine
  • Part Of: BAC One-Eleven, Design and development, airliner service
    powering both the BAC One-Eleven and Hawker Siddeley Trident
  • Part Of: Hawker Siddeley Trident, Design and development, airliner service (Trident)
    powering both the BAC One-Eleven and Hawker Siddeley Trident
  • Part Of: Blackburn Buccaneer, Tailored for the Buccaneer and Corsair II
    The Spey was chosen in 1960 as a re-engining option to give more thrust for a Buccaneer Mk.2.
  • Part Of: McDonnell Douglas F-4 Phantom II, F-4K and M Phantom
    The British versions of the McDonnell Douglas F-4 Phantom II (designated Phantom FG.Mk.1 and FGR.Mk.2) replaced the 16,000 lbf (71 kN) wet thrust J79 turbojets with a pair of 20,515 lbf (91 kN) wet thrust Spey 201 turbofans.
  • Part Of: Hawker Siddeley Nimrod, Applications
    Hawker Siddeley Nimrod MR1/R1/MR2/AEW3
  • Part Of: Fokker F28 Fellowship, Applications
    Fokker F28 Fellowship
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