Initial Operational Capability (IOC):
Also Known As: RD-600B and RD-600V
Parent System: RD-600
Initial Operational Capability (IOC): 2017
Total Production: ?
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Description: The NPO Saturn RD-600 is a turboshaft engine developed to power the Kamov Ka-60/Ka-62 twin-engine, multi-purpose helicopter. The engine provides between 1,000- and 1,550-hp. Both, the RD-600 and the TVD-1500 turboshafts, build upon the same gas generator which ensures high thermo-dynamic cycle parameters and components efficiency. The key elements of the RD-600 engine are its high reliability, modular design, monitoring and diagnosis system, and a full-authority digital electronic dual-channel control system with an auxiliary hydromechanical channel.
Service Life Flight Hours: 10,000
Emergency Power: 1,550 hp (1,156 kW)
Max Continuous Power: 1,000 hp (746 kW)
Max Power at TakeOff: 1,300 hp (970 kW)
Dry Weight: 220 kilogram (485 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)
Operators & Related Equipment
Grand Total ?1
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