The Soloviev D-20P, built by the Soloviev Design Bureau, was a low-bypass turbofan engine rated at 52.9 kN (11,900 lbf) thrust used on the Tupolev Tu-124. A later derivative with increased bypass ratio, the D-20P-125, was developed into the Soloviev D-30 family of low and medium bypass engines.[1]
D-20 | |
---|---|
![]() | |
Left side view of the Soloviev D-20 engine | |
Type | Turbofan |
Manufacturer | Soloviev Design Bureau |
Major applications | Tupolev Tu-124 |
Data from Aircraft engines of the World 1970[2]
Related lists
Aviadvigatel, Soloviev and Shvetsov aero engines | |
---|---|
Gas turbines | |
Radial engines |