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gptkbp:instance_of
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gptkb:aircraft
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|
gptkbp:air_traffic_control
|
manual control
|
|
gptkbp:aircraft_configuration
|
gptkb:monoplane
|
|
gptkbp:aircraft_operated
|
experimental
|
|
gptkbp:cockpit
|
single seat
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:decommissioned
|
gptkb:1960
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
Handley Page design team
|
|
gptkbp:design_date
|
gptkb:1955
|
|
gptkbp:design_purpose
|
research and development
|
|
gptkbp:engine_type
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gptkb:jet_engine
|
|
gptkbp:first_flight
|
gptkb:1957
gptkb:England
|
|
gptkbp:fuel_capacity
|
1,000 L
|
|
gptkbp:fuselage_material
|
gptkb:NACA_0012
|
|
gptkbp:height
|
3.81 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.111
|
|
gptkbp:influenced_by
|
H. P.115
|
|
gptkbp:landing_distance
|
600 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.80 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:max_takeoff_weight
|
3,175 kg
|
|
gptkbp:notable_pilots
|
gptkb:John_Farley
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:operational_history
|
used for research purposes
|
|
gptkbp:payload_capacity
|
500 kg
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:1960
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:stall_speed
|
120 km/h
|
|
gptkbp:successor
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:tail_type
|
gptkb:none
|
|
gptkbp:takeoff_distance
|
500 m
|
|
gptkbp:type
|
tailless aircraft
|
|
gptkbp:used_in
|
aerodynamics research
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wing_configuration
|
delta wing
|
|
gptkbp:wingspan
|
15.24 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|