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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
high-wing
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|
gptkbp:aircraft_operated
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gptkb:military_aircraft
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gptkbp:aircraft_role
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gptkb:transportation
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|
gptkbp:armament
|
gptkb:none
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|
gptkbp:cockpit
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pressurized
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|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
2
|
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gptkbp:crew_capacity
|
2
|
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gptkbp:design
|
gptkb:Bristol_Aeroplane_Company
gptkb:transportation
|
|
gptkbp:design_date
|
1950s
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|
gptkbp:engine_power
|
2,500 hp
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|
gptkbp:engine_type
|
gptkb:Bristol_Centaurus
|
|
gptkbp:first_flight
|
gptkb:1955
1955-07-01
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|
gptkbp:fuel_capacity
|
5,000 L
|
|
gptkbp:fuselage_material
|
monocoque
|
|
gptkbp:height
|
7.62 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Type 182
|
|
gptkbp:introduced
|
gptkb:1955
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|
gptkbp:landing_distance
|
800 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
22.86 m
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
|
gptkbp:max_speed
|
400 km/h
|
|
gptkbp:max_takeoff_weight
|
20,865 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:passenger_capacity
|
gptkb:20
|
|
gptkbp:payload_capacity
|
10,000 kg
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:production_location
|
gptkb:Bristol,_UK
|
|
gptkbp:production_years
|
1955-1960
|
|
gptkbp:propeller
|
gptkb:4
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:retirement_year
|
1960s
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:service_ceiling
|
6,100 m
|
|
gptkbp:service_entry
|
gptkb:1955
|
|
gptkbp:successor
|
gptkb:Bristol_Type_192
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
1,200 m
|
|
gptkbp:type
|
gptkb:transport_aircraft
|
|
gptkbp:used_by
|
gptkb:Royal_Air_Force
|
|
gptkbp:variant
|
Bristol Type 182 A
Bristol Type 182 B
|
|
gptkbp:wing_area
|
100 m²
|
|
gptkbp:wing_configuration
|
cantilever wing
|
|
gptkbp:wingspan
|
28.96 m
|
|
gptkbp:bfsParent
|
gptkb:Bristol_Siddeley_Orpheus
|
|
gptkbp:bfsLayer
|
7
|