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- Power_Jets_W.2 abstract "The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets (Research and Development) Ltd. Like the earlier Power Jets W.1, the trombone configuration featured a simple double-sided centrifugal compressor, reverse-flow combustion chambers and an air-cooled axial-flow turbine section.".
- Power_Jets_W.2 thumbnail Welland.JPG?width=300.
- Power_Jets_W.2 wikiPageExternalLink 1945%20-%202022.html.
- Power_Jets_W.2 wikiPageExternalLink 1962%20-%200757.html.
- Power_Jets_W.2 wikiPageID "24677697".
- Power_Jets_W.2 wikiPageLength "6841".
- Power_Jets_W.2 wikiPageOutDegree "39".
- Power_Jets_W.2 wikiPageRevisionID "695915903".
- Power_Jets_W.2 wikiPageWikiLink Afterburner.
- Power_Jets_W.2 wikiPageWikiLink Air_Ministry.
- Power_Jets_W.2 wikiPageWikiLink Category:Centrifugal-flow_turbojet_engines.
- Power_Jets_W.2 wikiPageWikiLink Category:Turbojet_engines_1940–1949.
- Power_Jets_W.2 wikiPageWikiLink Farnborough_Air_Sciences_Trust.
- Power_Jets_W.2 wikiPageWikiLink Fighter_aircraft.
- Power_Jets_W.2 wikiPageWikiLink Frank_Whittle.
- Power_Jets_W.2 wikiPageWikiLink Gloster_Aircraft_Company.
- Power_Jets_W.2 wikiPageWikiLink 39.
- Power_Jets_W.2 wikiPageWikiLink Gloster_Meteor.
- Power_Jets_W.2 wikiPageWikiLink List_of_Air_Ministry_specifications.
- Power_Jets_W.2 wikiPageWikiLink List_of_aircraft_engines.
- Power_Jets_W.2 wikiPageWikiLink Midland_Air_Museum.
- Power_Jets_W.2 wikiPageWikiLink Miles_M.52.
- Power_Jets_W.2 wikiPageWikiLink Power_Jets.
- Power_Jets_W.2 wikiPageWikiLink Power_Jets_W.1.
- Power_Jets_W.2 wikiPageWikiLink Ramjet.
- Power_Jets_W.2 wikiPageWikiLink Rolls-Royce_Meteor.
- Power_Jets_W.2 wikiPageWikiLink Rolls-Royce_Welland.
- Power_Jets_W.2 wikiPageWikiLink Rover_Company.
- Power_Jets_W.2 wikiPageWikiLink Royal_Air_Force_Museum_Cosford.
- Power_Jets_W.2 wikiPageWikiLink Turbofan.
- Power_Jets_W.2 wikiPageWikiLink Turbojet.
- Power_Jets_W.2 wikiPageWikiLink Vickers_Wellington.
- Power_Jets_W.2 wikiPageWikiLink File:Welland.JPG.
- Power_Jets_W.2 wikiPageWikiLinkText "Power Jets W.2".
- Power_Jets_W.2 wikiPageWikiLinkText "Power Jets W2/500".
- Power_Jets_W.2 wikiPageWikiLinkText "Power Jets W2/700".
- Power_Jets_W.2 wikiPageWikiLinkText "Power_Jets_W.2".
- Power_Jets_W.2 wikiPageWikiLinkText "Rover W2B".
- Power_Jets_W.2 wikiPageWikiLinkText "Rover W2B/#110".
- Power_Jets_W.2 wikiPageWikiLinkText "Rover W2B/23".
- Power_Jets_W.2 wikiPageWikiLinkText "Rover W2B/27".
- Power_Jets_W.2 wikiPageWikiLinkText "W.2".
- Power_Jets_W.2 wikiPageWikiLinkText "W2 700".
- Power_Jets_W.2 wikiPageWikiLinkText "Whittle W.2B".
- Power_Jets_W.2 wikiPageWikiLinkText "Whittle W2/700 Engine".
- Power_Jets_W.2 wikiPageWikiLinkText "Whittle W2B/23".
- Power_Jets_W.2 aircon "47".
- Power_Jets_W.2 combustion "Reverse flow can, 10 chambers".
- Power_Jets_W.2 compression "4".
- Power_Jets_W.2 compressor "Single-stage double-sided centrifugal flow".
- Power_Jets_W.2 developedFrom Power_Jets_W.1.
- Power_Jets_W.2 developedInto Rolls-Royce_Welland.
- Power_Jets_W.2 firstRun "c.".
- Power_Jets_W.2 fuelcon "2610".
- Power_Jets_W.2 fueltype "Kerosene".
- Power_Jets_W.2 lists "*List of aircraft engines".
- Power_Jets_W.2 majorApplications 39.
- Power_Jets_W.2 majorApplications Gloster_Meteor.
- Power_Jets_W.2 manufacturer Rover_Company.
- Power_Jets_W.2 ref "Jane's".
- Power_Jets_W.2 related "*Power Jets W.1 *Rolls-Royce Welland".
- Power_Jets_W.2 thrust "2485".
- Power_Jets_W.2 weight "2.6".
- Power_Jets_W.2 turbine "Single stage axial flow".
- Power_Jets_W.2 type Turbojet.
- Power_Jets_W.2 type "Centrifugal flow turbojet".
- Power_Jets_W.2 weight "950.0".
- Power_Jets_W.2 wikiPageUsesTemplate Template:Aircontent.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Avyear.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Cite_book.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Commons_category.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Convert.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Infobox_Aircraft_Engine.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Jetspecs.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Refbegin.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Refend.
- Power_Jets_W.2 wikiPageUsesTemplate Template:Reflist.
- Power_Jets_W.2 subject Category:Centrifugal-flow_turbojet_engines.
- Power_Jets_W.2 subject Category:Turbojet_engines_1940–1949.
- Power_Jets_W.2 hypernym Engine.
- Power_Jets_W.2 type Software.
- Power_Jets_W.2 comment "The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets (Research and Development) Ltd. Like the earlier Power Jets W.1, the trombone configuration featured a simple double-sided centrifugal compressor, reverse-flow combustion chambers and an air-cooled axial-flow turbine section.".
- Power_Jets_W.2 label "Power Jets W.2".
- Power_Jets_W.2 sameAs Q7236340.
- Power_Jets_W.2 sameAs Power_Jets_W.2.
- Power_Jets_W.2 sameAs m.080b8w_.
- Power_Jets_W.2 sameAs Q7236340.
- Power_Jets_W.2 wasDerivedFrom Power_Jets_W.2?oldid=695915903.
- Power_Jets_W.2 depiction Welland.JPG.
- Power_Jets_W.2 isPrimaryTopicOf Power_Jets_W.2.