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- WSK_SO-3 abstract "The WSK SO-1 and WSK-SO-3 are Polish turbojet engines designed by the Instytut Lotnictwa (Institute of Aeronautics ) and manufactured by WSK PZL Rzeszów, to power the PZL TS-11 Iskra jet trainer. Thirty SO-1s were built, this being superseded by the improved SO-3, of which a further 580 were built.The engine has a seven-stage compressor, annular combustion chambers, and a single-stage turbine.".
- WSK_SO-3 wikiPageID "25930999".
- WSK_SO-3 wikiPageRevisionID "589791158".
- WSK_SO-3 combustion "Annular with 24 combustors".
- WSK_SO-3 compression "4.8".
- WSK_SO-3 compressor "Seven-stage all-steel axial compressor".
- WSK_SO-3 diameter "707".
- WSK_SO-3 firstRun "November".
- WSK_SO-3 hasPhotoCollection WSK_SO-3.
- WSK_SO-3 length "2157.0".
- WSK_SO-3 lists "*List of aircraft engines".
- WSK_SO-3 majorApplications PZL_TS-11_Iskra.
- WSK_SO-3 manufacturer PZL.
- WSK_SO-3 nationalOrigin Poland.
- WSK_SO-3 numberBuilt "580".
- WSK_SO-3 ref "Jane's All The World's Aircraft 1988-89.".
- WSK_SO-3 similarEngines "*Armstrong Siddeley Viper".
- WSK_SO-3 thrust "10.8".
- WSK_SO-3 weight "3.4".
- WSK_SO-3 turbine "Single-stage axial flow".
- WSK_SO-3 type Turbojet.
- WSK_SO-3 weight "321.0".
- WSK_SO-3 subject Category:Turbojet_engines_1940–1949.
- WSK_SO-3 comment "The WSK SO-1 and WSK-SO-3 are Polish turbojet engines designed by the Instytut Lotnictwa (Institute of Aeronautics ) and manufactured by WSK PZL Rzeszów, to power the PZL TS-11 Iskra jet trainer. Thirty SO-1s were built, this being superseded by the improved SO-3, of which a further 580 were built.The engine has a seven-stage compressor, annular combustion chambers, and a single-stage turbine.".
- WSK_SO-3 label "WSK SO-3".
- WSK_SO-3 sameAs m.0b6hbf6.
- WSK_SO-3 sameAs Q7955733.
- WSK_SO-3 sameAs Q7955733.
- WSK_SO-3 wasDerivedFrom WSK_SO-3?oldid=589791158.
- WSK_SO-3 isPrimaryTopicOf WSK_SO-3.