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- SNECMA_14R abstract "The SNECMA 14R was a 14 cylinder two-row air-cooled radial engine developed in France from the Gnome-Rhône 14N, initially as the Gnome-Rhône 14R, with production after 1945 as the SNECMA 14R.".
- SNECMA_14R wikiPageID "33237355".
- SNECMA_14R wikiPageLength "3427".
- SNECMA_14R wikiPageOutDegree "11".
- SNECMA_14R wikiPageRevisionID "655508981".
- SNECMA_14R wikiPageWikiLink 100_octane.
- SNECMA_14R wikiPageWikiLink 92_Octane.
- SNECMA_14R wikiPageWikiLink Avgas.
- SNECMA_14R wikiPageWikiLink B.M.E.P..
- SNECMA_14R wikiPageWikiLink Breguet_500_Colmar.
- SNECMA_14R wikiPageWikiLink Breguet_Br_500_Colmar.
- SNECMA_14R wikiPageWikiLink Category:Radial_engines.
- SNECMA_14R wikiPageWikiLink France.
- SNECMA_14R wikiPageWikiLink Gnome-Rhône.
- SNECMA_14R wikiPageWikiLink Gnome-Rhône_14N.
- SNECMA_14R wikiPageWikiLink Gnome_et_Rhône.
- SNECMA_14R wikiPageWikiLink Mean_effective_pressure.
- SNECMA_14R wikiPageWikiLink Mercury_(element).
- SNECMA_14R wikiPageWikiLink Octane_rating.
- SNECMA_14R wikiPageWikiLink SNECMA.
- SNECMA_14R wikiPageWikiLink Snecma.
- SNECMA_14R wikiPageWikiLinkText "SNECMA 14R".
- SNECMA_14R componentsOther "Starter: Air equipment electric inertia starter * Ignition: 2 x R.B. magnetos, 2 x short reach spark plugs per cylinder fed by a shielded ignition harness.".
- SNECMA_14R compression "6.8".
- SNECMA_14R coolingsystem "Air-cooled with baffles".
- SNECMA_14R developedFrom Gnome-Rhône_14N.
- SNECMA_14R fuelsystem "1".
- SNECMA_14R fueltype "92".
- SNECMA_14R generalOther "Frontal Area:".
- SNECMA_14R hasPhotoCollection SNECMA_14R.
- SNECMA_14R majorApplications Breguet_500_Colmar.
- SNECMA_14R majorApplications Breguet_Br_500_Colmar.
- SNECMA_14R manufacturer Gnome-Rhône.
- SNECMA_14R manufacturer Gnome_et_Rhône.
- SNECMA_14R manufacturer SNECMA.
- SNECMA_14R manufacturer Snecma.
- SNECMA_14R nationalOrigin France.
- SNECMA_14R oilcon "0.0067".
- SNECMA_14R oilsystem "Pressure fed at".
- SNECMA_14R performanceOther "14".
- SNECMA_14R power "*Take-off: at 2,600 rpm at Hg boost with 100 octane fuel **Military, low: at 2,600 rpm at **Military, high: at 2,600 rpm at **Normal, low: at 2,400 rpm at **Normal, high: at 2,400 rpm at".
- SNECMA_14R weight "1.494".
- SNECMA_14R reductionGear "Planetary / epicyclic bevel reduction gearing at 0.67:1 ratio".
- SNECMA_14R specfuelcon "0.292".
- SNECMA_14R specpower "31.85".
- SNECMA_14R supercharger "Gear-driven 2-speed supercharger at 6.5:1 and 9.0:1 ratios".
- SNECMA_14R type "14".
- SNECMA_14R valvetrain "Single inlet and exhaust valves operated by rockers and pushrods".
- SNECMA_14R wikiPageUsesTemplate Template:Engineering-stub.
- SNECMA_14R wikiPageUsesTemplate Template:Infobox_aircraft_engine.
- SNECMA_14R wikiPageUsesTemplate Template:Pistonspecs.
- SNECMA_14R wikiPageUsesTemplate Template:Reflist.
- SNECMA_14R subject Category:Radial_engines.
- SNECMA_14R type Article.
- SNECMA_14R type Article.
- SNECMA_14R comment "The SNECMA 14R was a 14 cylinder two-row air-cooled radial engine developed in France from the Gnome-Rhône 14N, initially as the Gnome-Rhône 14R, with production after 1945 as the SNECMA 14R.".
- SNECMA_14R label "SNECMA 14R".
- SNECMA_14R sameAs m.0py0kc2.
- SNECMA_14R sameAs Q7391835.
- SNECMA_14R sameAs Q7391835.
- SNECMA_14R wasDerivedFrom SNECMA_14R?oldid=655508981.
- SNECMA_14R isPrimaryTopicOf SNECMA_14R.