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SNECMA M88)
The Snecma M88 is a French afterburning turbofan engine developed by Snecma for the Dassault Rafale fighter.
[edit] Applications
[edit] Specifications (M88-2)
Data from [1]
General characteristics
- Type: Twin-shaft, turbofan engine
- Length: 3,538 mm (139.3 in)
- Diameter: 900 mm (35.4 in) max
- Dry weight: 897 kg (1,977 lb)
Components
- Compressor: 3 stage low pressure, 6 stage high pressure
- Combustors: Annular
- Turbine: single stage high pressure, single stage low pressure
Performance
- Maximum thrust: 50 kN (11,250 lbf) dry, 75 kN (16,900 lbf) wet (afterburning)
- Overall pressure ratio: 24.5:1
- Bypass ratio: 0.3
- Turbine inlet temperature: 1,850K (2,870 °F)
- Fuel consumption: 0.80 kg/(daN*h) (0.78 lbm/(lbf*h)) (dry), 1.75 kg/(daN*h) (1.72 lbm/(lbf*hr)) (wet/afterburning)
- Thrust-to-weight ratio: 5.7:1 (dry), 8.5:1 (wet/afterburning)
[edit] See also
- Comparable engines
- Related lists
[edit] References
- ^ Desclaux, Jacques and Jacques Serre (2003). M88 – 2 E4: Advanced New Gengeration Engine for Rafale Multirole Fighter. AIAA/ICAS International Air and Space Symposium and Exposition: The Next 100 Years. 14–17 July 2003, Dayton, Ohio. AIAA 2003-2610.
[edit] External links
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