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M53-P2
IOC: 1985
Origin France
Contractor/s
Snecma
Applications
Mirage 2000-5 Mirage 2000B Mirage 2000C Mirage 2000D Mirage 2000N
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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.
Specifications
Dimensions: Diameter 800 mm, Length 5 m
Weights: Max Weight 1,515 kg (3,340 lb)
Engine/s Performance: Thrust 21,400 lb (9,707 kg)
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Notes
(*) lead contractor
IOC: Initial Operating Capability
FOC: Full Operating Capability
CEP: Circular Error Probable
Comm: Commissioning Date
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)
Last Updated: Saturday, November 22, 2008
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