gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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5
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gptkbp:bfsParent
|
gptkb:Avro_Shackleton
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gptkbp:armament
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gptkb:rocket
torpedoes
depth charges
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gptkbp:crew
|
gptkb:10
2
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gptkbp:engine_type
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gptkb:Rolls-Royce_Griffon
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gptkbp:first_flight
|
gptkb:1991
1951
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gptkbp:fuel_capacity
|
1,500 US gallons
|
https://www.w3.org/2000/01/rdf-schema#label
|
Shackleton AEW
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gptkbp:is_used_by
|
gptkb:military_base
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gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
30.5 m
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gptkbp:manufacturer
|
gptkb:Avro
|
gptkbp:max_speed
|
400 km/h
|
gptkbp:max_takeoff_weight
|
60,000 lb
|
gptkbp:notable_features
|
gptkb:radar_system
gptkb:aircraft
modular design
navigation systems
advanced avionics
surveillance systems
sonar equipment
sonobuoys
high altitude performance
searchlight
large cabin space
twin-engine configuration
emergency systems
electronic warfare capabilities
large payload capacity
cargo handling systems
crew comfort features
de-icing systems
high wing design
long endurance
|
gptkbp:number_built
|
gptkb:40
|
gptkbp:range
|
3,000 km
|
gptkbp:retired
|
gptkb:1991
|
gptkbp:role
|
gptkb:football_club
gptkb:mythological_figure
reconnaissance
anti-submarine warfare
surveillance
|
gptkbp:seating_capacity
|
8
20,000 lb
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gptkbp:service_ceiling
|
30,000 ft
|
gptkbp:services
|
gptkb:1955
|
gptkbp:successor
|
gptkb:Boeing_P-8_Poseidon
|
gptkbp:variant
|
gptkb:Shackleton_AEW.1
gptkb:Shackleton_MR.1
gptkb:Shackleton_MR.2
|
gptkbp:wing_area
|
200 m²
|
gptkbp:wingspan
|
30.2 m
|