Search results
Results from the WOW.Com Content Network
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 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 ...
For example, in Generation 1 and Generation 2 HSDs maximum speed is mainly limited by the speed of the smaller electric motor (often functioning as a generator). The Generation 3 HSD separates the ICE-MG1 path from the MG2 path, each with its own, tailored gear ratio (1.1:1 and 2.5:1, respectively, for late Priuses, including the Prius c).
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.
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.
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 .
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.
I'm currently working on Roland Beamont's article, and am currently intrigued to know which test pilot flew TSR-2 on its last flight on 31 March 1965. If you look at the table in this copy of Flight International) [ 1 ] it only lists the 23rd flight on 27 March 1965 piloted by Don Knight .