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"The trouble with the TSR-2 was that it tried to combine the most advanced state of every art in every field. The aircraft firms and the RAF were trying to get the Government on the hook and understated the cost. But TSR-2 cost far more than even their private estimates, and so I have no doubt about the decision to cancel."
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 TSR-2 had used a half-cone translating centre-body to change the direction. [20] Subsonic pressure recovery is addressed by removal of the boundary layer (at the ramp bleed slot) and suitable shaping of the subsonic diffuser leading to the engine. The pressure recovery achieved by Concorde's engine intakes at Mach 2 cruise gave an intake ...
TSR2 may refer to: the TSR2 (gene) , a human gene encoding a protein involved in ribosome biogenesis the BAC TSR-2 , British Aircraft Corporation Tactical Strike/Reconnaissance 2
Motor disorders are disorders of the nervous system that cause abnormal and involuntary movements. They can result from damage to the motor system. [1]Motor disorders are defined in the fifth edition of the Diagnostic and Statistical Manual of Mental Disorders (DSM-5) – published in 2013 to replace the fourth text revision – as a new sub-category of neurodevelopmental disorders.
Other problems may be implicated in the case of older vehicles equipped with carburetors. Weak, disconnected, or mis-connected throttle return springs, worn shot-pump barrels, chafed bowden cable housings, and cables which jump their tracks in the throttle-body crank can all cause similar acceleration problems.
The switched reluctance motor (SRM) is a type of reluctance motor. Unlike brushed DC motors , power is delivered to windings in the stator (case) rather than the rotor . This simplifies mechanical design because power does not have to be delivered to the moving rotor, which eliminates the need for a commutator .
At the end of World War II, the Bristol Engine Company's major effort was the development of the Hercules and Centaurus radial piston engines. By the end of 1946, the company had only 10 hours of turbojet experience with a small experimental engine called the Phoebus which was the gas generator or core of the Proteus turboprop then in development. [6]