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Turbojet development at the RAE information


Between 1936 and 1940 Alan Arnold Griffith designed a series of turbine engines that were built under the direction of Hayne Constant at the Royal Aircraft Establishment (RAE). The designs were advanced for the era, typically featuring a "two-spool" layout with high- and low-pressure compressors that individually had more stages than typical engines of the era. Although advanced, the engines were also difficult to build, and only the much simpler "Freda" design would ever see production, as the Metrovick F.2 and later the Armstrong Siddeley Sapphire. Much of the pioneering work would be later used in Rolls-Royce designs, starting with the hugely successful Rolls-Royce Avon.

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Turbojet development at the RAE

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that were built under the direction of Hayne Constant at the Royal Aircraft Establishment (RAE). The designs were advanced for the era, typically featuring...

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125 sq ft (11.6 m2) Airfoil: RAE 102 Gross weight: 4,500 lb (2,041 kg) Powerplant: 1 × Armstrong Siddeley Viper 101 turbojet engine, 1,640 lbf (7.3 kN)...

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invented the turbojet engine. A patent was submitted by Maxime Guillaume in 1921 for a similar invention which was technically unfeasible at the time. Whittle's...

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Power, 2002, p. 124, 542–549 Eckardt, Dietrich (2022). "Early Turbojet Developments in the USA and Other Countries". Jet Web. Wiesbaden, Germany: Springer...

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with four de Havilland Ghost turbojet engines buried in the wing roots, a pressurised cabin, and large windows. For the era, it offered a relatively quiet...

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up at R.A.E. Bedford. The two-seat 707C joined the R.A.E. in January 1956; perhaps its most substantial research contribution was to the development of...

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published. In it he talks about the needs for high-speed flight and the use of turbojets as the only reasonable solution to the problem of propeller efficiency...

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