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- Klimov_GTD-350 abstract "The Klimov GTD-350 (initially Isotov GTD-350) is a Soviet gas-turbine turboshaft engine intended for helicopter use. Designed in the early 1960s by the Isotov Design Bureau the engine was later produced by Klimov and PZL, production ending in the late 1990s.The GTD-350 powers the Mil Mi-2, the first Soviet gas-turbine powered helicopter, and has accumulated over 20 million hours in service.".
- Klimov_GTD-350 wikiPageID "35972324".
- Klimov_GTD-350 wikiPageLength "2676".
- Klimov_GTD-350 wikiPageOutDegree "13".
- Klimov_GTD-350 wikiPageRevisionID "668351902".
- Klimov_GTD-350 wikiPageWikiLink Allison_Model_250.
- Klimov_GTD-350 wikiPageWikiLink Category:Klimov_aircraft_engines.
- Klimov_GTD-350 wikiPageWikiLink Category:Turboshaft_engines_1960–1969.
- Klimov_GTD-350 wikiPageWikiLink Isotov_Design_Bureau.
- Klimov_GTD-350 wikiPageWikiLink Klimov.
- Klimov_GTD-350 wikiPageWikiLink List_of_aircraft_engines.
- Klimov_GTD-350 wikiPageWikiLink Mil_Mi-2.
- Klimov_GTD-350 wikiPageWikiLink PZL.
- Klimov_GTD-350 wikiPageWikiLink Turboshaft.
- Klimov_GTD-350 wikiPageWikiLinkText "Klimov GTD-350".
- Klimov_GTD-350 aircon "2.19".
- Klimov_GTD-350 combustion "Single-chamber reverse flow".
- Klimov_GTD-350 compression "6.05".
- Klimov_GTD-350 compressor "Seven-stage axial flow plus single-stage centrifugal".
- Klimov_GTD-350 hasPhotoCollection Klimov_GTD-350.
- Klimov_GTD-350 lists "* List of aircraft engines".
- Klimov_GTD-350 majorApplications Mil_Mi-2.
- Klimov_GTD-350 manufacturer Klimov.
- Klimov_GTD-350 weight "2.2".
- Klimov_GTD-350 ref "Klimov and Gunston.".
- Klimov_GTD-350 similarEngines "*Allison Model 250".
- Klimov_GTD-350 specfuelcon "365".
- Klimov_GTD-350 turbine "Single-stage compressor turbine, two-stage power turbine".
- Klimov_GTD-350 type Turboshaft.
- Klimov_GTD-350 type "Turboshaft".
- Klimov_GTD-350 wikiPageUsesTemplate Template:Aircontent.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Commons_category.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Jetspecs.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Klimov_aeroengines.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Refbegin.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Refend.
- Klimov_GTD-350 wikiPageUsesTemplate Template:Reflist.
- Klimov_GTD-350 subject Category:Klimov_aircraft_engines.
- Klimov_GTD-350 subject Category:Turboshaft_engines_1960–1969.
- Klimov_GTD-350 hypernym Engine.
- Klimov_GTD-350 type Software.
- Klimov_GTD-350 comment "The Klimov GTD-350 (initially Isotov GTD-350) is a Soviet gas-turbine turboshaft engine intended for helicopter use. Designed in the early 1960s by the Isotov Design Bureau the engine was later produced by Klimov and PZL, production ending in the late 1990s.The GTD-350 powers the Mil Mi-2, the first Soviet gas-turbine powered helicopter, and has accumulated over 20 million hours in service.".
- Klimov_GTD-350 label "Klimov GTD-350".
- Klimov_GTD-350 sameAs Klimov_GTD-350.
- Klimov_GTD-350 sameAs Isotow_GTD-350.
- Klimov_GTD-350 sameAs GTD–350.
- Klimov_GTD-350 sameAs GTD-350.
- Klimov_GTD-350 sameAs m.0j_6p_0.
- Klimov_GTD-350 sameAs Klimov_GTD-350.
- Klimov_GTD-350 sameAs Klimov_GTD-350.
- Klimov_GTD-350 sameAs Q626560.
- Klimov_GTD-350 sameAs Q626560.
- Klimov_GTD-350 wasDerivedFrom Klimov_GTD-350?oldid=668351902.
- Klimov_GTD-350 isPrimaryTopicOf Klimov_GTD-350.