Photo from the personal collection of Konstantinos Panitsidis
Technical specifications Photos Video
TECHNICAL SPECIFICATIONS
Fuel | TS-1, T-1 |
Oil | MK-8, MK-22, MK-20 |
Propeller shaft power, take-off power rating | 5.550 h.p. |
Specific fuel consumption, take-off power rating | 0,287 kg/h.p.*h |
Propeller shaft power, cruise power (H=1.000 m, V=250 km/h) | 3.100 h.p. |
Specific fuel consumption, cruise power | 0,343 kg/h.p.*h |
Pressure ratio, take-take-off power rating | 5,6 |
Temperature of the gas at the turbine intake, take-off power rating | 1.160 K |
Air flow rate, take-off power rating | 26 kg/h |
Compressor rotation frequency low-pressure, take-off power rating | 10.530 rpm. |
Diameter | 572 mm |
Height | 1158 mm |
Width | 1086 mm |
Lenght | 2737 mm |
Weight | 1.243 mm |
Specified service life | 6.000 h |