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SNECMA M88
From Wikipedia, the free encyclopedia
The M88 is an afterburning turbofan engine developed for the Dassault Rafale omnirole fighter by Snecma.
Although the M88 engine cycle is similar to that of the Eurojet EJ200, it is smaller and lower in thrust. Other differences are that the M88 has fan variable camber inlet guide vanes, the HP compressor has a 6th stage and the exhaust nozzle is of the ejector type. The M88 delivers 50 kN (11,250lbf) of dry thrust and 75 kN (17,000 lbf) on full reheat.
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