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- Turbomeca_TM_333 abstract "The Turbomeca TM 333 is a turboshaft engine designed for 5- to 6-ton-class helicopters. The TM 333 found its first commercial application on the HAL Dhruv.".
- Turbomeca_TM_333 wikiPageExternalLink sous_famille_home.php?sfid=505&mid=615.
- Turbomeca_TM_333 wikiPageID "1714934".
- Turbomeca_TM_333 wikiPageLength "2328".
- Turbomeca_TM_333 wikiPageOutDegree "18".
- Turbomeca_TM_333 wikiPageRevisionID "668326804".
- Turbomeca_TM_333 wikiPageWikiLink Axial_compressor.
- Turbomeca_TM_333 wikiPageWikiLink Aérospatiale_Alouette_III.
- Turbomeca_TM_333 wikiPageWikiLink Aérospatiale_SA_315B_Lama.
- Turbomeca_TM_333 wikiPageWikiLink Category:Turbomeca_aircraft_engines.
- Turbomeca_TM_333 wikiPageWikiLink Category:Turboshaft_engines_1970–1979.
- Turbomeca_TM_333 wikiPageWikiLink Centrifugal_compressor.
- Turbomeca_TM_333 wikiPageWikiLink France.
- Turbomeca_TM_333 wikiPageWikiLink Turbomeca_Shakti.
- Turbomeca_TM_333 wikiPageWikiLink HAL_Dhruv.
- Turbomeca_TM_333 wikiPageWikiLink Hindustan_Aeronautics_Limited.
- Turbomeca_TM_333 wikiPageWikiLink Turbomeca.
- Turbomeca_TM_333 wikiPageWikiLink Turboshaft.
- Turbomeca_TM_333 wikiPageWikiLinkText "TM 333-2B2".
- Turbomeca_TM_333 wikiPageWikiLinkText "Turbomeca TM 333".
- Turbomeca_TM_333 wikiPageWikiLinkText "Turbomeca TM 333-2B2".
- Turbomeca_TM_333 wikiPageWikiLinkText "Turbomeca TM333-2B".
- Turbomeca_TM_333 wikiPageWikiLinkText "Turbomeca TM333-2M2".
- Turbomeca_TM_333 breadth "450.0".
- Turbomeca_TM_333 combustion "Reverse annular flow".
- Turbomeca_TM_333 compression "10".
- Turbomeca_TM_333 compressor "2".
- Turbomeca_TM_333 firstRun "1974".
- Turbomeca_TM_333 fueltype "ATF K-50".
- Turbomeca_TM_333 length "1045.0".
- Turbomeca_TM_333 majorApplications HAL_Dhruv.
- Turbomeca_TM_333 manufacturer Turbomeca.
- Turbomeca_TM_333 nationalOrigin France.
- Turbomeca_TM_333 numberBuilt "250".
- Turbomeca_TM_333 oilUsed "MIL-L-23699".
- Turbomeca_TM_333 power "801.0".
- Turbomeca_TM_333 powerToWeightRatio "4.81".
- Turbomeca_TM_333 turbine "2".
- Turbomeca_TM_333 turbinetemp "1230.0".
- Turbomeca_TM_333 type Turboshaft.
- Turbomeca_TM_333 type "Turboshaft".
- Turbomeca_TM_333 weight "166.5".
- Turbomeca_TM_333 width "745.0".
- Turbomeca_TM_333 wikiPageUsesTemplate Template:Aeroengine-specs.
- Turbomeca_TM_333 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Turbomeca_TM_333 wikiPageUsesTemplate Template:Jetspecs.
- Turbomeca_TM_333 wikiPageUsesTemplate Template:Reflist.
- Turbomeca_TM_333 wikiPageUsesTemplate Template:Turbomeca_aeroengines.
- Turbomeca_TM_333 wikiPageUsesTemplate Template:Unreferenced.
- Turbomeca_TM_333 subject Category:Turbomeca_aircraft_engines.
- Turbomeca_TM_333 subject Category:Turboshaft_engines_1970–1979.
- Turbomeca_TM_333 hypernym Engine.
- Turbomeca_TM_333 type Software.
- Turbomeca_TM_333 comment "The Turbomeca TM 333 is a turboshaft engine designed for 5- to 6-ton-class helicopters. The TM 333 found its first commercial application on the HAL Dhruv.".
- Turbomeca_TM_333 label "Turbomeca TM 333".
- Turbomeca_TM_333 sameAs Q7853909.
- Turbomeca_TM_333 sameAs Turbomeca_TM_333.
- Turbomeca_TM_333 sameAs チュルボメカ_TM_333.
- Turbomeca_TM_333 sameAs m.05qlcl.
- Turbomeca_TM_333 sameAs Q7853909.
- Turbomeca_TM_333 wasDerivedFrom Turbomeca_TM_333?oldid=668326804.
- Turbomeca_TM_333 isPrimaryTopicOf Turbomeca_TM_333.