Search results
Results From The WOW.Com Content Network
The Rolls-Royce Olympus (originally the Bristol B.E.10 Olympus) was the world's second two-spool axial-flow turbojet aircraft engine design, first run in May 1950 and preceded only by the Pratt & Whitney J57, first-run in January 1950. [1] [2] It is best known as the powerplant of the Avro Vulcan and later models in the Concorde SST.
Olympus 593 on display at the Imperial War Museum Duxford. The Rolls-Royce/Snecma Olympus 593 was a reheated version of the Olympus which powered the supersonic airliner Concorde. [32] The Olympus 593 project was started in 1964, using the TSR2's Olympus Mk 320 as a basis for development. [33] BSEL and Snecma Moteurs of France were to share the ...
Gloster Aircraft had been studying a variety of updates and variations of the Javelin from before the first production model flew in 1953. These generated enough interest for the Air Ministry to ask for a version switching the Javelin's Armstrong Siddeley Sapphire engines for the more powerful Bristol Olympus.
The Gloster Javelin is a twin-engined all-weather interceptor aircraft designed and produced by the Gloster Aircraft Company. It was operated by the Royal Air Force from the mid-1950s until the late 1960s and was the final aircraft design to bear the Gloster name.
The Rolls-Royce/Snecma Olympus 593 was an Anglo-French turbojet with reheat, which powered the supersonic airliner Concorde.It was initially a joint project between Bristol Siddeley Engines Limited (BSEL) and Snecma, derived from the Bristol Siddeley Olympus 22R engine.
Pages in category "Bristol aircraft engines" The following 22 pages are in this category, out of 22 total. This list may not reflect recent changes. A. Bristol Aquila; C.
In effect, the aircraft would be built 50/50: Vickers the front half, EE the rear. [20] The TSR-2 was to be powered by two Bristol-Siddeley Olympus reheated turbojets, advanced variants of those used in the Avro Vulcan. The Olympus would be further developed and would power the supersonic Concorde. [68]
The thin wing design of the Type 213 was preferred by the STC and a 1961 contract encouraged a detailed series of studies of a 130-seat, Mach 2.2 aircraft powered by six Bristol Olympus engines under the generic Type 198 label. Aware of the great expense of the project, STAC required Bristol to share the cost with an overseas partner.