R11F2-300 Turbojet engine  © Konstantinos Panitsidis

Photo from the personal collection of Konstantinos Panitsidis


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TECHNICAL SPECIFICATIONS

Fuel -
Oil -
Max thrust take-off power rating 3.977 kgf
Specific fuel consumption, take-off power rating -
Max thrust, cruise power -
Specific fuel consumption, cruise power 0.94 kg/kgf. h
Pressure ratio, take-off power rating 8,8
Bypass ratio -
Temperature of the gas at the turbine intake, take-off power rating 1.175 K
Air flow rate, take-off power rating -
Compressor rotation frequency low-pressure, take-off power rating -
Compressor rotation frequency high-pressure, take-off power rating  
Diameter 900 mm
Height -
Width -
Length 4600 mm
Weight 1088,5 kg
Specified service life 1.500 h