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gptkbp:instanceOf
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aircraft
|
|
gptkbp:aircraft
|
fixed-wing aircraft
high-wing
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gptkbp:armament
|
none
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gptkbp:cockpit
|
tandem_seating
|
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gptkbp:constructionMaterial
|
3.05 m
|
|
gptkbp:controls
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elevators
ailerons
rudder
|
|
gptkbp:covers
|
slotted flaps
|
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gptkbp:crew
|
2
|
|
gptkbp:design
|
military logistics
military transport
high-wing configuration
Armstrong_Whitworth_design_team
|
|
gptkbp:enginePower
|
1,500 hp
|
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gptkbp:engineType
|
turboprop
|
|
gptkbp:financial_aid
|
longitudinal stability
directional stability
lateral stability
|
|
gptkbp:firstFlight
|
1960
1960-07-01
|
|
gptkbp:fuelCapacity
|
5,000 liters
|
|
gptkbp:headlights
|
T-tail
|
|
gptkbp:height
|
8.23 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Armstrong Whitworth A.W. 660
|
|
gptkbp:landingGear
|
tricycle gear
retractable landing gear
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:manufacturer
|
gptkb:Armstrong_Whitworth
|
|
gptkbp:maxSpeed
|
500 km/h
|
|
gptkbp:maxTakeoffWeight
|
20,865 kg
|
|
gptkbp:numberOfEpisodes
|
2
|
|
gptkbp:operationalHistory
|
used in various military operations
|
|
gptkbp:operationalRange
|
1,200 km
|
|
gptkbp:passengerCapacity
|
30
3,000 kg
|
|
gptkbp:primaryUser
|
gptkb:Royal_Air_Force
|
|
gptkbp:productionYears
|
1960-1965
|
|
gptkbp:propulsion
|
variable-pitch propeller
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retirementYear
|
1970
|
|
gptkbp:role
|
transport aircraft
|
|
gptkbp:services
|
7,620 m
|
|
gptkbp:successor
|
gptkb:Armstrong_Whitworth_A.W._660C
|
|
gptkbp:takeoffDistance
|
1,200 m
1,000 m
|
|
gptkbp:totalGoals
|
50
|
|
gptkbp:variant
|
A.W. 660A
A.W. 660B
|
|
gptkbp:wingArea
|
70 m²
|
|
gptkbp:wingspan
|
25.91 m
|