|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
swept wing
|
|
gptkbp:armament
|
cannons
missiles
|
|
gptkbp:avionics
|
basic instrumentation
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:commissioningDate
|
1950s
|
|
gptkbp:constructionMaterial
|
metal
|
|
gptkbp:controls
|
elevators
ailerons
rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
aerodynamic efficiency
high speed
performance-oriented
Armstrong_Whitworth_design_team
|
|
gptkbp:engineType
|
turbofan
|
|
gptkbp:firstFlight
|
1955
|
|
gptkbp:fuelCapacity
|
3,000 L
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historicalSignificance
|
advanced design for its time
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W.83
|
|
gptkbp:influencedBy
|
Cold_War_dynamics
|
|
gptkbp:influences
|
jet technology
|
|
gptkbp:inheritsFrom
|
A.W.81
|
|
gptkbp:inspiration
|
post-war aviation needs
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced future designs
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
1,100 km/h
|
|
gptkbp:maxTakeoffWeight
|
15,000 kg
|
|
gptkbp:notableFeature
|
none
advanced aerodynamics
swept wings
high thrust-to-weight ratio
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:productionCompany
|
conceptual
not produced
|
|
gptkbp:range
|
2,000 km
|
|
gptkbp:relatedAircraft
|
gptkb:Armstrong_Whitworth_A.W.52
|
|
gptkbp:relatedPatent
|
A.W.94
|
|
gptkbp:role
|
fighter aircraft
interceptor
|
|
gptkbp:services
|
15,000 m
not entered service
|
|
gptkbp:successor
|
none
|
|
gptkbp:targetMarket
|
military aviation
|
|
gptkbp:weight
|
8,000 kg
|
|
gptkbp:wingspan
|
14.63 m
|