Rolls-Royce/Snecma M45h (Paperback)

Please note that the content of this book primarily consists of articles available from Wikipedia or other free sources online. The Rolls-Royce/SNECMA M45H was a medium bypass ratio turbofan produced specifically for the twin-engined VFW-Fokker 614 aircraft in the early 1970s.The design was started as a collaborative effort between Bristol Siddeley and SNECMA.The single-stage fan, together with a five-stage LP compressor, was driven by a three-stage LP turbine, whilst the seven-stage HP compressor was driven by a single-stage, air-cooled, HP turbine. An annular combustor and an unmixed exhaust, with a plug-type primary nozzle, were other design features.