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gptkbp:instance_of
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gptkb:aircraft
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|
gptkbp:air_traffic_control
|
hydraulic
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|
gptkbp:aircraft_configuration
|
gptkb:monoplane
|
|
gptkbp:aircraft_operated
|
experimental
|
|
gptkbp:aspect_ratio
|
3.5
|
|
gptkbp:avionics
|
analog
|
|
gptkbp:cockpit
|
enclosed
|
|
gptkbp:color_scheme
|
white and blue
|
|
gptkbp:configuration
|
tailless
|
|
gptkbp:control_surfaces
|
spoilers
flaps
slats
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:decommissioned
|
1955-01-01
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:design_date
|
gptkb:1952
|
|
gptkbp:design_purpose
|
aerodynamic research
|
|
gptkbp:elevation_control
|
elevons
|
|
gptkbp:emergency_services
|
gptkb:parachute
|
|
gptkbp:engine_configuration
|
rear-mounted
|
|
gptkbp:engine_type
|
gptkb:jet_engine
|
|
gptkbp:first_flight
|
1953
1953-06-01
|
|
gptkbp:fuselage_material
|
aluminum
delta wing
|
|
gptkbp:height
|
2.74 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.112
|
|
gptkbp:landing_distance
|
400 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.84 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:max_takeoff_weight
|
3,175 kg
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:notable_pilots
|
gptkb:John_Derry
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:power_source
|
gptkb:Rolls-Royce_Avon
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:1955
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
differential thrust
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:stall_speed
|
120 km/h
|
|
gptkbp:tail_type
|
gptkb:none
|
|
gptkbp:takeoff_distance
|
300 m
|
|
gptkbp:type
|
subsonic aircraft
|
|
gptkbp:wing_area
|
20.5 m²
|
|
gptkbp:wing_configuration
|
aluminum
|
|
gptkbp:wingspan
|
10.67 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|