gptkbp:instance_of
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gptkb:aircraft
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gptkbp:air_traffic_control
|
manual control
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gptkbp:aircraft_configuration
|
twin-engine
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gptkbp:aircraft_operated
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gptkb:aircraft
|
gptkbp:armament
|
gptkb:none
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gptkbp:cockpit
|
single-seat
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gptkbp:control_surfaces
|
elevators and ailerons
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gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
gptkbp:crew
|
gptkb:1
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gptkbp:decommissioned
|
1960s
|
gptkbp:design
|
Handley Page design team
Handley Page engineers
|
gptkbp:design_date
|
1950s
|
gptkbp:design_features
|
swept wings
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gptkbp:design_location
|
gptkb:Cricklewood,_London
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gptkbp:design_purpose
|
research into supersonic flight
|
gptkbp:engine
|
gptkb:Rolls-Royce
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Avon
gptkb:jet_engine
|
gptkbp:first_flight
|
gptkb:RAF_Boscombe_Down
1953
|
gptkbp:fuel_capacity
|
1,500 liters
|
gptkbp:fuselage_material
|
low-wing
|
gptkbp:height
|
3.96 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page HP.117
|
gptkbp:influenced_by
|
British jet technology
|
gptkbp:landing_distance
|
1,000 m
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
12.19 m
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
gptkbp:max_speed
|
800 km/h
|
gptkbp:max_takeoff_weight
|
5,000 kg
|
gptkbp:notable_features
|
high speed performance
|
gptkbp:notable_pilots
|
gptkb:John_Derry
|
gptkbp:number_built
|
gptkb:1
|
gptkbp:number_of_engines
|
2
|
gptkbp:predecessor
|
gptkb:Handley_Page_HP.115
|
gptkbp:primary_function
|
research and development
|
gptkbp:range
|
1,500 km
|
gptkbp:related_aircraft
|
gptkb:Handley_Page_Victor
gptkb:Handley_Page_Halifax
gptkb:Handley_Page_Hastings
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:service_ceiling
|
12,000 m
|
gptkbp:status
|
gptkb:prototype
|
gptkbp:successor
|
gptkb:Handley_Page_HP.115
|
gptkbp:tail_type
|
T-tail
|
gptkbp:takeoff_distance
|
1,200 m
|
gptkbp:type
|
gptkb:fighter_aircraft
|
gptkbp:used_for
|
aerodynamic testing
|
gptkbp:wing_area
|
34 m²
|
gptkbp:wingspan
|
15.24 m
|
gptkbp:bfsParent
|
gptkb:Handley_Page_H._P.119
|
gptkbp:bfsLayer
|
7
|