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- Microturbo_TRI_40 abstract "The Microturbo TRI-40 is a small turbojet engine developed for use in cruise missiles and small unmanned aerial vehicles in the 2.2 - 3.6 kN (500 - 800 lbf) thrust class.".
- Microturbo_TRI_40 wikiPageID "24762893".
- Microturbo_TRI_40 wikiPageLength "4018".
- Microturbo_TRI_40 wikiPageOutDegree "22".
- Microturbo_TRI_40 wikiPageRevisionID "668346151".
- Microturbo_TRI_40 wikiPageWikiLink Category:Turbojet_engines_1990–1999.
- Microturbo_TRI_40 wikiPageWikiLink Combustor.
- Microturbo_TRI_40 wikiPageWikiLink Cruise_missile.
- Microturbo_TRI_40 wikiPageWikiLink Electronic_control_unit.
- Microturbo_TRI_40 wikiPageWikiLink Exocet.
- Microturbo_TRI_40 wikiPageWikiLink France.
- Microturbo_TRI_40 wikiPageWikiLink Gas_compressor.
- Microturbo_TRI_40 wikiPageWikiLink JP-8.
- Microturbo_TRI_40 wikiPageWikiLink JP10.
- Microturbo_TRI_40 wikiPageWikiLink List_of_aircraft_engines.
- Microturbo_TRI_40 wikiPageWikiLink Magnet.
- Microturbo_TRI_40 wikiPageWikiLink Microturbo_TRI_60.
- Microturbo_TRI_40 wikiPageWikiLink Naval_Strike_Missile.
- Microturbo_TRI_40 wikiPageWikiLink Royal_Norwegian_Navy.
- Microturbo_TRI_40 wikiPageWikiLink Turbojet.
- Microturbo_TRI_40 wikiPageWikiLink Turbomeca.
- Microturbo_TRI_40 wikiPageWikiLink Unmanned_aerial_vehicle.
- Microturbo_TRI_40 wikiPageWikiLink Williams_F107.
- Microturbo_TRI_40 wikiPageWikiLinkText "Microturbo TRI 40".
- Microturbo_TRI_40 combustion Combustor.
- Microturbo_TRI_40 compressor "4".
- Microturbo_TRI_40 developedFrom Microturbo_TRI_60.
- Microturbo_TRI_40 diameter "280.0".
- Microturbo_TRI_40 firstRun "June 1999".
- Microturbo_TRI_40 fueltype JP-8.
- Microturbo_TRI_40 fueltype JP10.
- Microturbo_TRI_40 length "680.0".
- Microturbo_TRI_40 lists "*List of aircraft engines".
- Microturbo_TRI_40 majorApplications Naval_Strike_Missile.
- Microturbo_TRI_40 manufacturer Turbomeca.
- Microturbo_TRI_40 nationalOrigin France.
- Microturbo_TRI_40 similarEngines "*Williams F107".
- Microturbo_TRI_40 thrust "2.5".
- Microturbo_TRI_40 weight "5.7".
- Microturbo_TRI_40 turbine "Single-stage".
- Microturbo_TRI_40 turbinetemp "1010.0".
- Microturbo_TRI_40 type "Single Spool Turbojet".
- Microturbo_TRI_40 unitCost "100000.0".
- Microturbo_TRI_40 weight "44.0".
- Microturbo_TRI_40 wikiPageUsesTemplate Template:Aircontent.
- Microturbo_TRI_40 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Microturbo_TRI_40 wikiPageUsesTemplate Template:Jetspecs.
- Microturbo_TRI_40 wikiPageUsesTemplate Template:Microturbo_aeroengines.
- Microturbo_TRI_40 wikiPageUsesTemplate Template:Reflist.
- Microturbo_TRI_40 subject Category:Turbojet_engines_1990–1999.
- Microturbo_TRI_40 hypernym Engine.
- Microturbo_TRI_40 type Software.
- Microturbo_TRI_40 comment "The Microturbo TRI-40 is a small turbojet engine developed for use in cruise missiles and small unmanned aerial vehicles in the 2.2 - 3.6 kN (500 - 800 lbf) thrust class.".
- Microturbo_TRI_40 label "Microturbo TRI 40".
- Microturbo_TRI_40 sameAs Q17098935.
- Microturbo_TRI_40 sameAs Microturbo_TRI_40.
- Microturbo_TRI_40 sameAs m.080q8sf.
- Microturbo_TRI_40 sameAs Q17098935.
- Microturbo_TRI_40 wasDerivedFrom Microturbo_TRI_40?oldid=668346151.
- Microturbo_TRI_40 isPrimaryTopicOf Microturbo_TRI_40.