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gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
bomber
|
|
gptkbp:armament
|
machine guns
bombs
|
|
gptkbp:cockpit
|
open cockpit
|
|
gptkbp:crew
|
3
|
|
gptkbp:decommissioned
|
1940
|
|
gptkbp:design
|
gptkb:Sir_W.G._Armstrong_Whitworth
biplane
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Kestrel_V
|
|
gptkbp:engineType
|
gptkb:Rolls-Royce_Kestrel
|
|
gptkbp:firstFlight
|
1935
|
|
gptkbp:height
|
3.8 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W. 75
|
|
gptkbp:introduced
|
1936
|
|
gptkbp:landingGear
|
fixed landing gear
|
|
gptkbp:length
|
12.5 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
400 km/h
|
|
gptkbp:nationalTeam
|
gptkb:United_Kingdom
|
|
gptkbp:numberBuilt
|
approximately 100
|
|
gptkbp:produces
|
1935-1940
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1940
|
|
gptkbp:role
|
training aircraft
reconnaissance aircraft
light bomber
|
|
gptkbp:services
|
gptkb:Royal_Air_Force
6,000 m
|
|
gptkbp:successor
|
gptkb:Armstrong_Whitworth_A.W._38
|
|
gptkbp:usedBy
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
A.W. 75A
A.W. 75B
|
|
gptkbp:weight
|
3,000 kg
|
|
gptkbp:wingArea
|
40 m²
|
|
gptkbp:wingspan
|
15.2 m
|