Friday, January 09, 2009

Aktai

IOC: 2009

Origin
Russia

Program Status:
Under Development

Contractor/s
Kazan Helicopters

Description: The Kazan Helicopters Aktai is a light, single-engine, three-seat multi-purpose helicopter developed to suit a wide spectrum of duties in the commercial range. A single VAZ-3265 piston engine rated at 270-hp at takeoff drives a three-bladed main rotor allowing the aircraft to achieve a maximum airspeed of 190 kph. The cabin flexibility allows to accommodate up to four passengers including the pilot, one pilot and two passengers or one pilot and up to 300 kg of cargo in the rear compartment.

The Aktai design focuses on simplicity and low operating costs. Currently, Aktai is undergoing flight tests with the first helicopter rolling off the production line at Kazan Helicopters planned for 2009.

Specifications
Accommodation: Crew 1, Passengers 3

Dimensions: Cargo Compartment Length 1.2 m, Cargo Compartment Width 1 m

Weights: Cargo Hook Capacity 240 kg (529 lb), Max Weight 1,150 kg (2,535 lb), Payload 300 kg (661 lb)

Performance: Cabin Height 1.3 m (4 ft), Ceiling 4,700 m (15,420 ft), Cruise Speed 155 kph (96 mph), Hovering Ceiling 1,300 m (4,265 ft), Max Range 400 km (216 nm), Top Speed 190 kph (118 mph)

Power: Max Power at TakeOff 270 hp

Other: Main Rotor Blades 3, Number of Engines 1

Image Gallery

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Internet Resources
kazanhelicopters.ru

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, December 20, 2008

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