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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
military aircraft
single-engine
interceptor
straight wing
cantilever wing
prototype fighter
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:climbRate
|
8 m/s
|
|
gptkbp:cockpit
|
enclosed
|
|
gptkbp:commissioningDate
|
1938
|
|
gptkbp:constructionMaterial
|
NACA 2412
|
|
gptkbp:controls
|
elevators
ailerons
rudder
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:Sir_W.G._Armstrong_Whitworth
speed and agility
low-wing monoplane
|
|
gptkbp:engine
|
1
nose-mounted
|
|
gptkbp:enginePower
|
1,030 hp
|
|
gptkbp:engineType
|
gptkb:Rolls-Royce_Merlin
|
|
gptkbp:firstFlight
|
1939
1939-07-01
|
|
gptkbp:fuelCapacity
|
300 L
|
|
gptkbp:height
|
2.74 m
|
|
gptkbp:historicalSignificance
|
early_British_fighter_development
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W.51
|
|
gptkbp:influences
|
World_War_II_aircraft_design
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
500 km/h
|
|
gptkbp:maxTakeoffWeight
|
120 km/h
2,500 kg
|
|
gptkbp:numberBuilt
|
1
|
|
gptkbp:primaryUser
|
gptkb:Royal_Air_Force
|
|
gptkbp:productionCompany
|
1939-1940
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
800 km
|
|
gptkbp:relatedAircraft
|
gptkb:Armstrong_Whitworth_A.W.52
|
|
gptkbp:retirementYear
|
1940
|
|
gptkbp:role
|
fighter aircraft
|
|
gptkbp:serviceHistory
|
limited service
|
|
gptkbp:services
|
10,000 m
|
|
gptkbp:speed
|
70 km/h
|
|
gptkbp:status
|
prototype
|
|
gptkbp:succeededBy
|
30°/s
|
|
gptkbp:takeoffDistance
|
90 km/h
|
|
gptkbp:team
|
Armstrong_Whitworth_design_team
|
|
gptkbp:wingArea
|
20.5 m²
|
|
gptkbp:wingspan
|
10.67 m
|