Rafale and Snecma M-88-2 engine

Engine structure :

Twin-shaft, bypass turbofan engine

3-stage LP compressor with intel guide vane

6-stage HP compressor (3 stages with variable stator vanes)

Annular combustion chamber

Single-stage cooled HP turbine

Single-stage cooled LP turbine

Radial A/B chamber

Variable-section convergent flap-type nozzle

Full authority digital engine control(FADEC)

Modular on-condition maintenance(21modules)