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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
experimental
|
|
gptkbp:aircraft_type
|
gptkb:aircraft
|
|
gptkbp:climb_rate
|
1,500 ft/min
|
|
gptkbp:cockpit
|
tandem seating
|
|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:country
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
delta wing
|
|
gptkbp:design_purpose
|
research and development
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1957
1957-08-01
|
|
gptkbp:flaps
|
slotted flaps
|
|
gptkbp:fuselage_material
|
gptkb:NACA_0012
aluminum
|
|
gptkbp:height
|
3.96 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.116
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.19 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
300 knots
|
|
gptkbp:max_takeoff_weight
|
10,000 kg
|
|
gptkbp:members
|
3°/s
|
|
gptkbp:notable_pilots
|
gptkb:John_Farley
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:propulsion
|
gptkb:jet_engine
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:1960
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
30,000 ft
|
|
gptkbp:stall_speed
|
70 knots
|
|
gptkbp:strikeouts
|
4°/s
|
|
gptkbp:successor
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:used_for
|
aerodynamic research
|
|
gptkbp:weight
|
5,000 kg
8,000 kg
|
|
gptkbp:wing_area
|
40 m²
|
|
gptkbp:wing_configuration
|
composite
high wing
|
|
gptkbp:wingspan
|
15.24 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|