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The first reheat variant, the Bristol Siddeley Olympus Mk 320, powered the cancelled BAC TSR-2 supersonic strike aircraft. For Concorde, this was developed during the 1960s into the Rolls-Royce/Snecma Olympus 593, being further developed through several subsequent versions to eventually provide reliable airline service. The Olympus 593 is a ...
With new engines, the TSR-2 XR219 flew another 23 times before the project was cancelled in 1965. [30] By this time the engine had accumulated 6,000 hours of testing, including 800 hours of operation in reheat, with an additional 61 flight hours in the Vulcan test bed, and a further additional 26 flight hours in the TSR-2 prototype XR219 .
The British Aircraft Corporation TSR-2 is a cancelled Cold War strike and reconnaissance aircraft developed by the British Aircraft Corporation (BAC), for the Royal Air Force (RAF) in the late 1950s and early 1960s.
The 22R had been designed for sustained (45 minutes) flight at Mach 2.2 [3] as the engine for the BAC TSR-2. The 591 was redesigned, being known as the 593, with specification finalised on 1 January 1964. [1] Bristol Siddeley of the UK and Snecma Moteurs of France were to share the project.
Scheduled services commenced on 21 January 1976 on both the London–Bahrain and Paris–Rio de Janeiro routes. [14] The protototype BAC TSR-2 at the Warton factory in 1966. In 1963, BAC acquired the previously autonomous guided weapons divisions of English Electric and Bristol to form a new subsidiary, British Aircraft Corporation (Guided ...
TSR-2 XR220 at RAF Museum Cosford, 2002. Ferranti developed the first terrain-following radar specifically for the TSR-2. Terrain-following radar (TFR) is a military aerospace technology that allows a very-low-flying aircraft to automatically maintain a relatively constant altitude above ground level and therefore make detection by enemy radar more difficult.
Mode 1 schematic Input-split mode — C1 engaged; [23]: col.8 ll.57–59 the rotational speed of the 2nd motor (MG-B) is always proportional to the output shaft, while the 1st motor (MG-A) is not proportional to the input shaft. The 2nd electric motor direct drive the output, and it is possible to drive the vehicle without combustion engine.
Martin-Baker Mk.8 is the designation given to two distinct British ejection seat types designed and built by Martin-Baker.The original use applies to a seat developed for the cancelled BAC TSR-2 strike aircraft project of the 1960s, re-use of the designation applies to a lightweight version of the Martin-Baker Mk.10 seat for the Short Tucano and other similar military training aircraft.