Friday, August 29, 2008

AI-450

Origin:Russia

Contractor/s: Ivchenko-Progress, Motor Sich

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).

Specifications
Dimensions: Height 536 mm, Length 1,085 mm, Width 515 mm

Weights: Dry Weight 103 kg (227 lb)

Power: Max Continuous Power 300 hp, Max Power at TakeOff 465 hp

Other: Service Life (Flight Hours) 12,000

Applications
Ka-226 Operators

Russia

Image Gallery

Internet Resources
ivchenko-progress.com

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: Sunday, August 24, 2008

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