D-30KP-2

The NPO Saturn D-30KP-2 gas turbine engine is installed on aircraft of the IL-76 family (transport - IL-76 TD, IL-76 MD, fire-fighting - IL-76TP, IL-78 MK tanker aircraft, early warning aircraft A -50; amphibious aircraft A-40).

Engine characteristics:

Fan diameter, mm - 1455

Engine delivery weight - 3004 Air consumption, kg / s - 280

Takeoff (ISA, H = 0, M = 0): Traction, KGS - 12000

Specific fuel consumption, kg / kg.h - 0.51

Turbine inlet temperature, K - 1410

Cruise mode (H = 11 km, M = 0.8): Traction, KGS - 2750

Specific fuel consumption, kg / kgf - 0.71

Turbine inlet temperature, K - 1225