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- Soloviev_D-20 abstract "The Soloviev D-20P was a low-bypass turbofan engine rated at 52.9 kN (11,900 lbf) thrust. It was built by the Soloviev Design Bureau. The engine was used on the Tupolev Tu-124.".
- Soloviev_D-20 wikiPageID "17617086".
- Soloviev_D-20 wikiPageRevisionID "603382671".
- Soloviev_D-20 aircon "113".
- Soloviev_D-20 bypass "1".
- Soloviev_D-20 combustion "12".
- Soloviev_D-20 compression "13".
- Soloviev_D-20 compressor "Three-stage LP, eight-stage HP, axial flow".
- Soloviev_D-20 hasPhotoCollection Soloviev_D-20.
- Soloviev_D-20 lists "* List of aircraft engines".
- Soloviev_D-20 majorApplications Tupolev_Tu-124.
- Soloviev_D-20 manufacturer Soloviev_Design_Bureau.
- Soloviev_D-20 ref "Gunston.".
- Soloviev_D-20 thrust "5400.0".
- Soloviev_D-20 turbine "Two-stage LP turbine, single-stage HP turbine".
- Soloviev_D-20 type Turbofan.
- Soloviev_D-20 type "Twin-spool turbofan engine".
- Soloviev_D-20 weight "1468.0".
- Soloviev_D-20 subject Category:Low-bypass_turbofan_engines.
- Soloviev_D-20 subject Category:Soloviev_aircraft_engines.
- Soloviev_D-20 subject Category:Turbofan_engines_1950–1959.
- Soloviev_D-20 comment "The Soloviev D-20P was a low-bypass turbofan engine rated at 52.9 kN (11,900 lbf) thrust. It was built by the Soloviev Design Bureau. The engine was used on the Tupolev Tu-124.".
- Soloviev_D-20 label "Soloviev D-20".
- Soloviev_D-20 label "Solowjow D-20".
- Soloviev_D-20 label "ソロヴィヨーフ D-20".
- Soloviev_D-20 sameAs Solowjow_D-20.
- Soloviev_D-20 sameAs Soloviev_D-20.
- Soloviev_D-20 sameAs ソロヴィヨーフ_D-20.
- Soloviev_D-20 sameAs m.0464x_m.
- Soloviev_D-20 sameAs Q175481.
- Soloviev_D-20 sameAs Q175481.
- Soloviev_D-20 wasDerivedFrom Soloviev_D-20?oldid=603382671.
- Soloviev_D-20 isPrimaryTopicOf Soloviev_D-20.