gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:aircraft_configuration
|
twin-boom
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
gptkbp:aircraft_role
|
research and testing
|
gptkbp:aircraft_type
|
experimental supersonic aircraft
|
gptkbp:ceiling
|
15,000 m
|
gptkbp:cockpit
|
tandem
|
gptkbp:crew
|
2
|
gptkbp:decommissioned
|
gptkb:1964
|
gptkbp:design
|
gptkb:Bristol_Aeroplane_Company
tailless
|
gptkbp:design_date
|
gptkb:1955
|
gptkbp:design_features
|
swept wings
|
gptkbp:design_influence
|
gptkb:Concorde
|
gptkbp:engine_configuration
|
rear-mounted
|
gptkbp:engine_power
|
10,000 lbf
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Avon
twin-engine
|
gptkbp:first_flight
|
gptkb:1960
gptkb:10
gptkb:1964
gptkb:Bristol_Airport
1960-06-02
|
gptkbp:fuselage_material
|
gptkb:metal
|
gptkbp:height
|
4.57 m
|
gptkbp:historical_role
|
supersonic research
|
gptkbp:historical_significance
|
early supersonic flight research
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Type 188
|
gptkbp:influenced_by
|
gptkb:Bristol_175_Britannia
|
gptkbp:landing_distance
|
5,500 kg
|
gptkbp:landing_gear
|
gptkb:Cycling
|
gptkbp:length
|
15.24 m
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
gptkbp:max_speed
|
1,000 km/h
|
gptkbp:max_takeoff_weight
|
6,000 kg
|
gptkbp:nationality
|
gptkb:United_Kingdom
|
gptkbp:notable_features
|
variable-sweep wings
|
gptkbp:notable_pilots
|
gptkb:John_Farley
|
gptkbp:number_built
|
2
|
gptkbp:number_of_engines
|
2
|
gptkbp:operational_use
|
gptkb:none
|
gptkbp:project
|
Bristol 188 project
|
gptkbp:range
|
1,500 km
|
gptkbp:related_aircraft
|
Bristol 188
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:status
|
retired
|
gptkbp:successor
|
gptkb:none
|
gptkbp:tail_type
|
gptkb:none
|
gptkbp:used_for
|
research and development
|
gptkbp:wing_area
|
50 m²
|
gptkbp:wing_configuration
|
gptkb:metal
|
gptkbp:wingspan
|
15.24 m
|
gptkbp:year
|
gptkb:1955
gptkb:1964
|
gptkbp:bfsParent
|
gptkb:Bristol_aircraft_family
gptkb:Bristol_Siddeley_Olympus
|
gptkbp:bfsLayer
|
6
|