|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:air_traffic_control
|
manual control
|
|
gptkbp:aircraft_configuration
|
delta wing
|
|
gptkbp:aircraft_operated
|
retired
experimental military aircraft
|
|
gptkbp:aircraft_role
|
gptkb:aircraft
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:design_date
|
1950s
|
|
gptkbp:design_features
|
swept wings
|
|
gptkbp:design_influence
|
later delta wing aircraft
|
|
gptkbp:design_purpose
|
research and development
|
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Avon
gptkb:jet_engine
|
|
gptkbp:first_flight
|
gptkb:1957
successful
1957-09-01
|
|
gptkbp:fuel_capacity
|
1,500 liters
|
|
gptkbp:height
|
3.96 m
|
|
gptkbp:historical_context
|
Cold War era
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.108
|
|
gptkbp:landing_gear
|
tricycle landing gear
|
|
gptkbp:length
|
12.19 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
480 km/h
|
|
gptkbp:max_takeoff_weight
|
3,175 kg
|
|
gptkbp:notable_pilots
|
gptkb:John_Farley
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_history
|
limited
|
|
gptkbp:production_status
|
gptkb:prototype
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:related_aircraft
|
gptkb:Handley_Page_Victor
gptkb:Handley_Page_Halifax
gptkb:Handley_Page_H._P.115
|
|
gptkbp:retired
|
gptkb:1960
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:significance
|
aerodynamic research
|
|
gptkbp:stall_speed
|
100 km/h
|
|
gptkbp:type
|
tailless aircraft
|
|
gptkbp:used_by
|
gptkb:Royal_Air_Force
|
|
gptkbp:wing_area
|
40.5 m²
|
|
gptkbp:wingspan
|
15.24 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|