M53-P2

M53-P2

Initial Operational Capability (IOC): 1985
Total Production: ?
Origin: France
Corporations: Snecma

Parent System: M53-P2
Initial Operational Capability (IOC): 1985
Total Production: ?

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Description: The M53 is a combat proven engine designed to power the entire Mirage 2000 multi-role fighter family. It features high reliability, controllability with full authority digital control, and a modular design which provides easy maintainability. The M53 engine entered service in 1983.

More than 617 M53 engines have been delivered worldwide logging over 930,000 flight hours. The M53-P2 entered service in 1985 and has been chosen by eight air forces in four continents. Snecma is developing the M53-PX3 engine with improved reliability, full authority digital control, lower operation costs, and more thrust. The M53 engines will be in service well beyond 2025.

M53-P2 Applications

Combat Aircraft Mirage 2000-5 Mirage 2000B Mirage 2000C Mirage 2000D Mirage 2000N

M53-P2 Specifications

Dimensions
Fan Diameter: 800 millimeter (31.5 inch)
Length: 5.07 meter (200 inch)
Weight
Dry Weight: 1,515 kilogram (3,340 pound)
Thrust: 21,400 pound (9.71 ton)

CEP: Circular Error Probable
Meters (m) Kilometers (km) Nautic Miles (nm) Inch (in) Yard (yd) Foot (ft) Millimeter (mm)
Pound (lb) Kilogram (kg) kN (KiloNewton) Ton (t)
Meters per Second (mps) Kilometers per Hour (kph) Knot (kt) Miles per Hour (mph)
Liter (l) Galon (gl)
Year (yr) Minutes (min) Second (sec)
Shaft-Horse-Power (shp)