Friday, November 21, 2008

Ka-60 Kasatka

Ka-62

Origin
Russia

Contractor/s
Kamov

Family Members
Ka-60 Kasatka

Power plant:
RD-600V (2)

Description: The Ka-62 is a civil version of the Ka-60 military assault/transport helicopter developed by Kamov. It retains the single five-bladed main rotor, a 11-bladed tail rotor and wide side doors from the Ka-60. The Ka-62 is powered by two NPO Saturn RD-600V turboshaft engines. The helicopter's cabin can accommodate up to 16 passengers including two pilots. Overall, results slightly lighter and has greater range and better flight performance than the Ka-60.

Specifications
Accommodation: Crew 2, Passengers 14

Weights: Max Weight 6,250 kg (13,779 lb), Payload 2,000 kg (4,409 lb) inside or 2,500 kg underslung

Performance: Ceiling 5,500 m (18,045 ft), Cruise Speed 270 kph (168 mph), Hovering Ceiling 3,000 m (9,843 ft), Max Range 780 km (421 nm), Top Speed 300 kph (186 mph)

Other: Main Rotor Blades 5

Image Gallery

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, October 25, 2008

Leave Feedback >>