Snecma M88

Turbofan · SNECMA
Reaction Turbines
Maximum Takeoff Thrust
50 kN
Bypass Ratio
0.3
Diameter
696 mm
Length
3538 mm
Dry Weight
897 kg
Thrust To Weight
5.68

Architecture

Fan Fan Stages — Fan Blades — Fan Technology — Fan Pressure Ratio —
Gearbox Geared Fan No Gear — Reduction Ratio —
LP compressor Low-Pressure Compressor Stages — Low-Pressure Compressor Technology — BP Compressor Pressure Ratio —
IP compressor Intermediary-Pressure Compressor Stages — Intermediary-Pressure Compressor Technology — IP Compressor Pressure Ratio —
HP compressor High-Pressure Compressor Stages — High-Pressure Compressor Technology — HP Compressor Pressure Ratio —
Combustor Combustion Chamber Annular
HP turbine High Pressure Compressor Stages — High-Pressure Turbine Technology —
IP turbine Intermediary-Pressure Turbine Stages — Intermediary-Pressure Turbine Technology —
LP turbine Low-Pressure Turbine Stages — Low-Pressure Turbine Technology —
Whole engine Streams 2 Bypass Ratio 0.3 Overall Pressure Ratio — Afterburner Yes

Pictures

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Airplanes

Name Aircraft Engine Number of Engines Length (m) Flat Wing Span (m)
Dassault Rafale Snecma M88 2 15.27 10.9

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio
Volvo RM12 Volvo Aero 54 0.31 Compare
IHI Corporation XF5 IHI Corporation 49 Compare
Lyulka AL-5 Lyulka-Saturn 52 Compare
Pratt & Whitney J57 Pratt & Whitney 52 Compare
Tumansky R-21 Tumansky 46.1 Compare
Klimov RD-33 Klimov 50 0.49 Compare
All data (17 fields)
Name
Snecma M88
Aircraft Engine Manufacturer
SNECMA
Aircraft Engine Type
Turbofan
Dry Weight (kg)
897
Diameter (mm)
696
Length (mm)
3538
Wikipedia Article (URL)
en.wikipedia.org/wiki/Snecma_M88
Geared Fan
No
Combustion Chamber
Annular
Afterburner
Yes
Streams
2
Bypass Ratio
0.3
Maximum Takeoff Thrust (kN)
50
Thrust To Weight
5.68
Afterburner Thrust (kN)
50
Compressor Description
Axial, 3-stage LP, 6-stage HP
Turbine Description
1-stage LP, 1-stage HP