D-20 by Soloviev
First Soviet twin-spool bypass turbojet (turbofan) engine.
Model
D-20
Year
1959?
Type
bypass turbojet
Takeoff
Thrust
5400
kg
Fuel consumption
?
kg/kgf/hour
Cruise
Thrust
1100
kg
Fuel consumption
0.9
kg/kgf/hour
other parameters
Bypass ratio
?
Compression
?
Maximum turbine inlet temperature
°K
Resource
?
h
Length
?
mm
Maximum Diameter
?
mm
Weight
?
kg
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