There is 1 images added on 4 March 2007
Initial Operational Capability (IOC):
Total Production: ?
Origin: Russia
Corporations: Ivchenko-Progress and Motor Sich
Parent System: AI-450
Initial Operational Capability (IOC):
Total Production: ?
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Description: The Ivchenko-Progress AI-450 aircraft turboshaft engine has been designed to power single- and twin-engine helicopters in the 1.5 to 4 tons maximum takeoff weight range such as Ka-226, Mi-2A and Ansat. The engine features modular design which translates into simplified assembly and overhaul. Ivchenko-Progress along with Motor Sich are developing several versions with higher power output (AI-450-2), turboprop engine (AI-450TP) and auxiliary power unit (AI-450MS).

AI-450 Applications

Private Aircraft Ka-226

AI-450 Specifications

Service Life Flight Hours: 12,000
Height: 536 millimeter (21.1 inch)
Length: 1,085 millimeter (43 inch)
Width: 515 millimeter (20.3 inch)
Max Continuous Power: 300 hp (224 kW)
Max Power at TakeOff: 465 hp (347 kW)
Dry Weight: 103 kilogram (227 pound)
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)

Operators & Related Equipment


Grand Total ?1
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