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- Nord_1601 abstract "The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation. The aircraft was designed to investigate the aerodynamics of swept wings and related high-lift devices.".
- Nord_1601 manufacturer Nord_Aviation.
- Nord_1601 numberBuilt "1".
- Nord_1601 wikiPageID "17260950".
- Nord_1601 wikiPageLength "3774".
- Nord_1601 wikiPageOutDegree "20".
- Nord_1601 wikiPageRevisionID "668355158".
- Nord_1601 wikiPageWikiLink 1950_in_aviation.
- Nord_1601 wikiPageWikiLink Aileron.
- Nord_1601 wikiPageWikiLink Cantilever.
- Nord_1601 wikiPageWikiLink Category:French_experimental_aircraft_1950–1959.
- Nord_1601 wikiPageWikiLink Category:Nord_aircraft.
- Nord_1601 wikiPageWikiLink Cockpit.
- Nord_1601 wikiPageWikiLink Ejection_seat.
- Nord_1601 wikiPageWikiLink France.
- Nord_1601 wikiPageWikiLink Landing_gear.
- Nord_1601 wikiPageWikiLink Leading_edge.
- Nord_1601 wikiPageWikiLink Martin-Baker.
- Nord_1601 wikiPageWikiLink Monoplane.
- Nord_1601 wikiPageWikiLink Nord_Aviation.
- Nord_1601 wikiPageWikiLink Rolls-Royce_Derwent.
- Nord_1601 wikiPageWikiLink Trailing_edge.
- Nord_1601 wikiPageWikiLink Turbojet.
- Nord_1601 wikiPageWikiLinkText "Nord 1601".
- Nord_1601 ceilingFt "39370".
- Nord_1601 ceilingM "12000".
- Nord_1601 crew "1".
- Nord_1601 emptyWeightKg "4710".
- Nord_1601 emptyWeightLb "10384".
- Nord_1601 eng1Kn "17.8".
- Nord_1601 eng1Lbf "4000".
- Nord_1601 eng1Number "2".
- Nord_1601 eng1Type "Rolls-Royce Derwent 5 turbojet".
- Nord_1601 firstFlight "1950-01-24".
- Nord_1601 grossWeightKg "6700".
- Nord_1601 heightFt "12".
- Nord_1601 heightIn "0".
- Nord_1601 heightM "3.67".
- Nord_1601 lengthFt "38".
- Nord_1601 lengthIn "7".
- Nord_1601 lengthM "11.62".
- Nord_1601 manufacturer Nord_Aviation.
- Nord_1601 maxSpeedKmh "1000".
- Nord_1601 maxSpeedMph "621".
- Nord_1601 metOrEng%3F_ "met".
- Nord_1601 nationalOrigin "France".
- Nord_1601 numberBuilt "1".
- Nord_1601 rangeKm "1135".
- Nord_1601 rangeMiles "705".
- Nord_1601 ref "Gaillard p.110".
- Nord_1601 spanFt "40".
- Nord_1601 spanIn "10".
- Nord_1601 spanM "12.4".
- Nord_1601 type "Aerodynamic research aircraft".
- Nord_1601 wikiPageUsesTemplate Template:Aerospecs.
- Nord_1601 wikiPageUsesTemplate Template:Aircontent.
- Nord_1601 wikiPageUsesTemplate Template:Cite_book.
- Nord_1601 wikiPageUsesTemplate Template:Commons_category.
- Nord_1601 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Nord_1601 wikiPageUsesTemplate Template:Nord_aircraft.
- Nord_1601 wikiPageUsesTemplate Template:Reflist.
- Nord_1601 wingAreaSqft "333".
- Nord_1601 wingAreaSqm "30.2".
- Nord_1601 subject Category:French_experimental_aircraft_1950–1959.
- Nord_1601 subject Category:Nord_aircraft.
- Nord_1601 hypernym Aircraft.
- Nord_1601 type Aircraft.
- Nord_1601 type MeanOfTransportation.
- Nord_1601 type Product.
- Nord_1601 type DesignedArtifact.
- Nord_1601 type Thing.
- Nord_1601 type Q11436.
- Nord_1601 comment "The Nord 1601 was a French aerodynamic research aircraft designed and built by Nord Aviation. The aircraft was designed to investigate the aerodynamics of swept wings and related high-lift devices.".
- Nord_1601 label "Nord 1601".
- Nord_1601 sameAs Q7050534.
- Nord_1601 sameAs Nord_1601.
- Nord_1601 sameAs Nord_1601.
- Nord_1601 sameAs m.043n1_s.
- Nord_1601 sameAs Q7050534.
- Nord_1601 wasDerivedFrom Nord_1601?oldid=668355158.
- Nord_1601 isPrimaryTopicOf Nord_1601.