|
gptkbp:instanceOf
|
aircraft
|
|
gptkbp:aircraft
|
gptkb:delta_wing
experimental aircraft
9,000 kg
twin-engine configuration
experimental supersonic aircraft
|
|
gptkbp:airlines
|
30 minutes
|
|
gptkbp:avionics
|
advanced avionics suite
|
|
gptkbp:countryOfOrigin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Bristol_Type_188
1960s
variable geometry wings
Bristol_Aeroplane_Company_team
|
|
gptkbp:engine
|
Bristol_Orpheus_engine
|
|
gptkbp:engineType
|
twin-engine
|
|
gptkbp:firstFlight
|
1962
1962-07-02
conducted in 1962
|
|
gptkbp:hasArea
|
gptkb:John_Farley
|
|
gptkbp:height
|
4.57 m
|
|
gptkbp:historicalSignificance
|
early supersonic research
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Bristol Type 188
|
|
gptkbp:influenced
|
gptkb:Concorde
|
|
gptkbp:legacy
|
pioneering supersonic research
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Bristol_Aeroplane_Company
|
|
gptkbp:maxSpeed
|
1,000 km/h
|
|
gptkbp:maxTakeoffWeight
|
10,000 kg
|
|
gptkbp:missions
|
fly-by-wire system
|
|
gptkbp:numberBuilt
|
2
|
|
gptkbp:operationalArea
|
none
|
|
gptkbp:passengerCapacity
|
0
|
|
gptkbp:performance
|
high-speed performance metrics
|
|
gptkbp:project
|
1964
Bristol_Type_188_project
|
|
gptkbp:relatedAircraft
|
Bristol_Type_167
|
|
gptkbp:relatedPatent
|
British_supersonic_transport
|
|
gptkbp:releaseYear
|
1961-12-01
|
|
gptkbp:retired
|
1964
|
|
gptkbp:role
|
experimental aircraft
research aircraft
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:session
|
aerodynamic research
|
|
gptkbp:significance
|
supersonic flight research
|
|
gptkbp:status
|
retired
|
|
gptkbp:type
|
supersonic aircraft
|
|
gptkbp:wingArea
|
supersonic flight envelope
|
|
gptkbp:wingspan
|
15.24 m
|