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- Armstrong_Whitworth_AW.171 abstract "The Armstrong Whitworth AW.171 was a British project of the 1950s to develop a supersonic VTOL flying wing aircraft. It was planned to investigate the extremely low aspect ratio delta wings proposed by Professor A.A. Griffith for supersonic transports. The A.W.171 design was a very slender delta flying wing powered by two Bristol Orpheus turbojets mounted at the wingtips, with 10 Rolls-Royce RB.108 lift jets. The pilot was to lie in a prone position to minimise drag. Work was cancelled in 1957 before a prototype was completed.".
- Armstrong_Whitworth_AW.171 manufacturer Armstrong_Whitworth.
- Armstrong_Whitworth_AW.171 wikiPageExternalLink UK-AW.htm.
- Armstrong_Whitworth_AW.171 wikiPageID "14096474".
- Armstrong_Whitworth_AW.171 wikiPageRevisionID "572911146".
- Armstrong_Whitworth_AW.171 crew "1".
- Armstrong_Whitworth_AW.171 eng1LbfAb "4850".
- Armstrong_Whitworth_AW.171 eng1Name Bristol_Siddeley_Orpheus.
- Armstrong_Whitworth_AW.171 eng1Number "2".
- Armstrong_Whitworth_AW.171 eng1Type Turbojet.
- Armstrong_Whitworth_AW.171 eng2Lbf "2100".
- Armstrong_Whitworth_AW.171 eng2Name Rolls-Royce_RB108.
- Armstrong_Whitworth_AW.171 eng2Number "10".
- Armstrong_Whitworth_AW.171 eng2Type "turbojet".
- Armstrong_Whitworth_AW.171 grossWeightLb "17500".
- Armstrong_Whitworth_AW.171 hasPhotoCollection Armstrong_Whitworth_AW.171.
- Armstrong_Whitworth_AW.171 lengthFt "70".
- Armstrong_Whitworth_AW.171 lengthIn "10".
- Armstrong_Whitworth_AW.171 manufacturer Armstrong_Whitworth.
- Armstrong_Whitworth_AW.171 maxSpeedMach "2".
- Armstrong_Whitworth_AW.171 numberBuilt "none".
- Armstrong_Whitworth_AW.171 primeUnits%3F_ "imp".
- Armstrong_Whitworth_AW.171 ref "Paper Planes:Armstrong Whitworth's unbuilt projects".
- Armstrong_Whitworth_AW.171 similarAircraft "*Bristol 188".
- Armstrong_Whitworth_AW.171 spanFt "17".
- Armstrong_Whitworth_AW.171 spanIn "7".
- Armstrong_Whitworth_AW.171 status "cancelled".
- Armstrong_Whitworth_AW.171 type "Experimental aircraft".
- Armstrong_Whitworth_AW.171 subject Category:Aircraft_with_auxiliary_jet_engines.
- Armstrong_Whitworth_AW.171 subject Category:Armstrong_Whitworth_aircraft.
- Armstrong_Whitworth_AW.171 subject Category:British_experimental_aircraft_1950–1959.
- Armstrong_Whitworth_AW.171 subject Category:Cancelled_aircraft_projects.
- Armstrong_Whitworth_AW.171 subject Category:Delta-wing_aircraft.
- Armstrong_Whitworth_AW.171 subject Category:Flying_wings.
- Armstrong_Whitworth_AW.171 subject Category:Twinjets.
- Armstrong_Whitworth_AW.171 subject Category:VTOL_aircraft.
- Armstrong_Whitworth_AW.171 type Aircraft.
- Armstrong_Whitworth_AW.171 type MeanOfTransportation.
- Armstrong_Whitworth_AW.171 type Product.
- Armstrong_Whitworth_AW.171 type Model_airplane.
- Armstrong_Whitworth_AW.171 type DesignedArtifact.
- Armstrong_Whitworth_AW.171 comment "The Armstrong Whitworth AW.171 was a British project of the 1950s to develop a supersonic VTOL flying wing aircraft. It was planned to investigate the extremely low aspect ratio delta wings proposed by Professor A.A. Griffith for supersonic transports. The A.W.171 design was a very slender delta flying wing powered by two Bristol Orpheus turbojets mounted at the wingtips, with 10 Rolls-Royce RB.108 lift jets. The pilot was to lie in a prone position to minimise drag.".
- Armstrong_Whitworth_AW.171 label "Armstrong Whitworth AW.171".
- Armstrong_Whitworth_AW.171 sameAs m.03ctgz_.
- Armstrong_Whitworth_AW.171 sameAs Q4794010.
- Armstrong_Whitworth_AW.171 sameAs Q4794010.
- Armstrong_Whitworth_AW.171 wasDerivedFrom Armstrong_Whitworth_AW.171?oldid=572911146.
- Armstrong_Whitworth_AW.171 isPrimaryTopicOf Armstrong_Whitworth_AW.171.