Takeoff power
(H = 0; Mn = 0; Standard atmospheric conditions +15 °C)
efficiency.....14000 hp
specific fuel consumption .....0,170 kg/hp *h
Maximum cruise power
(H= 11000m) Mn = 0.7, standard atmospheric conditions)
efficiency .....6750 hp
specific fuel consumption .....0.130 kg/hp*h
prop-fan net efficiency, more .....0,9
Prop-fan diameter .....4,5 m
Engine dry mass (less prop-fan) .....1650 kg