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- MTR_MTR390 abstract "The MTU Turbomeca Rolls-Royce MTR390 is a turboshaft developed for light helicopter applications by MTU Turbomeca Rolls-Royce (MTR). The engine is designed to power helicopters in the weight range of 5-7 tonnes in both single and twin engine configurations. So far the only application is the Eurocopter Tiger. Test runs of the MTR390 began in 1989 and the first test flight was performed in 1991. The MTR390 received military certification in May 1996 and civil approval in June 1997.An uprated version, the MTR390-E (Enhanced), is being developed with Spain's ITP.".
- MTR_MTR390 wikiPageExternalLink MTR390-turboshaft-helicopter-engines.
- MTR_MTR390 wikiPageExternalLink mtr390e.pdf.
- MTR_MTR390 wikiPageExternalLink www.mtr390.com.
- MTR_MTR390 wikiPageExternalLink index.html.
- MTR_MTR390 wikiPageExternalLink mtr390-48.
- MTR_MTR390 wikiPageID "596290".
- MTR_MTR390 wikiPageLength "2912".
- MTR_MTR390 wikiPageOutDegree "17".
- MTR_MTR390 wikiPageRevisionID "668340426".
- MTR_MTR390 wikiPageWikiLink 1989_in_aviation.
- MTR_MTR390 wikiPageWikiLink 1991_in_aviation.
- MTR_MTR390 wikiPageWikiLink 1996_in_aviation.
- MTR_MTR390 wikiPageWikiLink 1997_in_aviation.
- MTR_MTR390 wikiPageWikiLink Category:Turboshaft_engines_1980–1989.
- MTR_MTR390 wikiPageWikiLink Centrifugal_compressor.
- MTR_MTR390 wikiPageWikiLink Combustor.
- MTR_MTR390 wikiPageWikiLink Eurocopter_Tiger.
- MTR_MTR390 wikiPageWikiLink Industria_de_Turbo_Propulsores.
- MTR_MTR390 wikiPageWikiLink MTU_Turbomeca_Rolls-Royce.
- MTR_MTR390 wikiPageWikiLink Turboshaft.
- MTR_MTR390 wikiPageWikiLinkText "MTR MTR390".
- MTR_MTR390 wikiPageWikiLinkText "MTR390".
- MTR_MTR390 combustion Combustor.
- MTR_MTR390 compression "13".
- MTR_MTR390 compressor "Centrifugal, 2 stage".
- MTR_MTR390 diameter "26.8".
- MTR_MTR390 firstRun "December 1989".
- MTR_MTR390 hasPhotoCollection MTR_MTR390.
- MTR_MTR390 length "42.4".
- MTR_MTR390 majorApplications Eurocopter_Tiger.
- MTR_MTR390 manufacturer MTU_Turbomeca_Rolls-Royce.
- MTR_MTR390 power "1465".
- MTR_MTR390 specfuelcon "0.46".
- MTR_MTR390 turbine "1".
- MTR_MTR390 type Centrifugal_compressor.
- MTR_MTR390 type Turboshaft.
- MTR_MTR390 weight "372.0".
- MTR_MTR390 wikiPageUsesTemplate Template:Commons_category.
- MTR_MTR390 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- MTR_MTR390 wikiPageUsesTemplate Template:Jetspecs.
- MTR_MTR390 wikiPageUsesTemplate Template:Joint_development_aeroengines.
- MTR_MTR390 wikiPageUsesTemplate Template:Reflist.
- MTR_MTR390 subject Category:Turboshaft_engines_1980–1989.
- MTR_MTR390 hypernym Turboshaft.
- MTR_MTR390 comment "The MTU Turbomeca Rolls-Royce MTR390 is a turboshaft developed for light helicopter applications by MTU Turbomeca Rolls-Royce (MTR). The engine is designed to power helicopters in the weight range of 5-7 tonnes in both single and twin engine configurations. So far the only application is the Eurocopter Tiger. Test runs of the MTR390 began in 1989 and the first test flight was performed in 1991.".
- MTR_MTR390 label "MTR MTR390".
- MTR_MTR390 sameAs Category:MTR390.
- MTR_MTR390 sameAs MTR390.
- MTR_MTR390 sameAs MTR_MTR390.
- MTR_MTR390 sameAs MTR_390.
- MTR_MTR390 sameAs MTR390.
- MTR_MTR390 sameAs m.02ts0d.
- MTR_MTR390 sameAs MTR_MTR390.
- MTR_MTR390 sameAs Q1325950.
- MTR_MTR390 sameAs Q1325950.
- MTR_MTR390 wasDerivedFrom MTR_MTR390?oldid=668340426.
- MTR_MTR390 homepage www.mtr390.com.
- MTR_MTR390 isPrimaryTopicOf MTR_MTR390.