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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
air superiority
military aircraft
monoplane
150 kg/m²
|
|
gptkbp:armament
|
machine guns
|
|
gptkbp:climbRate
|
10 m/s
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|
gptkbp:cockpit
|
forward
enclosed
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|
gptkbp:commissioningDate
|
1936
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gptkbp:constructionMaterial
|
NACA 2412
|
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gptkbp:controls
|
elevators
ailerons
rudder
|
|
gptkbp:crew
|
1
|
|
gptkbp:design
|
gptkb:R._J._Mitchell
speed and agility
low-wing configuration
|
|
gptkbp:developer
|
gptkb:Armstrong_Whitworth_A.W._45
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Merlin
|
|
gptkbp:engineType
|
liquid-cooled
|
|
gptkbp:firstFlight
|
1938
|
|
gptkbp:fuelCapacity
|
200 liters
|
|
gptkbp:hasArea
|
gptkb:John_W._B._Smith
|
|
gptkbp:headlights
|
conventional tail
|
|
gptkbp:height
|
2.74 m
|
|
gptkbp:historicalSignificance
|
prototype_for_British_fighters.
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W. 46
|
|
gptkbp:landingGear
|
tricycle gear
|
|
gptkbp:length
|
8.23 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
500 km/h
|
|
gptkbp:nationalTeam
|
gptkb:United_Kingdom
|
|
gptkbp:numberBuilt
|
1
|
|
gptkbp:productionYears
|
1938
|
|
gptkbp:propulsion
|
two-bladed
0.15 kW/kg
|
|
gptkbp:range
|
800 km
|
|
gptkbp:relatedAircraft
|
gptkb:Supermarine_Spitfire
|
|
gptkbp:role
|
fighter aircraft
interceptor
|
|
gptkbp:services
|
8000 m
not entered service
|
|
gptkbp:speed
|
90 km/h
|
|
gptkbp:status
|
prototype
|
|
gptkbp:takeoffDistance
|
300 m
400 m
|
|
gptkbp:type
|
single-engine
|
|
gptkbp:wingArea
|
6.0
|
|
gptkbp:wingspan
|
10.67 m
|