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- Tumansky_R-21 abstract "The Tumansky R-21 was a Russian turbojet engine of the 1960s. Used for development only, the project was canceled.".
- Tumansky_R-21 wikiPageID "29593099".
- Tumansky_R-21 wikiPageRevisionID "491574332".
- Tumansky_R-21 compressor "Six-stage axial compressor".
- Tumansky_R-21 developedFrom Tumansky_R-11.
- Tumansky_R-21 diameter "987.0".
- Tumansky_R-21 firstRun "1960".
- Tumansky_R-21 hasPhotoCollection Tumansky_R-21.
- Tumansky_R-21 lists "*List of aircraft engines".
- Tumansky_R-21 majorApplications Mikoyan-Gurevich_Ye-8.
- Tumansky_R-21 manufacturer Sergei_Tumansky.
- Tumansky_R-21 related "*Tumansky R-11".
- Tumansky_R-21 thrust "*46.1 kN military power *70.6 kN with afterburner".
- Tumansky_R-21 type Turbojet.
- Tumansky_R-21 type "Afterburning turbojet".
- Tumansky_R-21 weight "1250.0".
- Tumansky_R-21 subject Category:Tumansky_aircraft_engines.
- Tumansky_R-21 subject Category:Turbojet_engines_1960–1969.
- Tumansky_R-21 comment "The Tumansky R-21 was a Russian turbojet engine of the 1960s. Used for development only, the project was canceled.".
- Tumansky_R-21 label "Tumansky R-21".
- Tumansky_R-21 sameAs m.0fpgvn6.
- Tumansky_R-21 sameAs Q7852496.
- Tumansky_R-21 sameAs Q7852496.
- Tumansky_R-21 wasDerivedFrom Tumansky_R-21?oldid=491574332.
- Tumansky_R-21 isPrimaryTopicOf Tumansky_R-21.