|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:air_traffic_control
|
fly-by-wire
|
|
gptkbp:aspect_ratio
|
5.0
|
|
gptkbp:avionics
|
analog instruments
|
|
gptkbp:climb_rate
|
15 m/s
|
|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:design_features
|
canard configuration
swept wings
delta wing
high-mounted wings
twin-engine configuration
|
|
gptkbp:design_purpose
|
research and development
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Avon
|
|
gptkbp:engine_type
|
turbojet
|
|
gptkbp:first_flight
|
gptkb:1957
1957-07-01
|
|
gptkbp:fuel_capacity
|
1,500 L
|
|
gptkbp:fuselage_material
|
gptkb:NACA_0012
|
|
gptkbp:height
|
3.96 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page HP.118
|
|
gptkbp:landing_distance
|
150 km/h
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.19 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:max_takeoff_weight
|
5,000 kg
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:passenger_capacity
|
gptkb:0
|
|
gptkbp:power_source
|
2 × Rolls-Royce Avon engines
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:related_aircraft
|
gptkb:Handley_Page_Victor
gptkb:Handley_Page_Halifax
gptkb:Handley_Page_Hastings
gptkb:Handley_Page_HP.115
|
|
gptkbp:retirement_year
|
gptkb:1960
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:service_entry
|
gptkb:1958
|
|
gptkbp:stall_speed
|
120 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:takeoff_distance
|
180 km/h
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wing_configuration
|
166.67 kg/m²
|
|
gptkbp:wingspan
|
15.24 m
|
|
gptkbp:bfsParent
|
gptkb:Handley_Page_H._P.119
|
|
gptkbp:bfsLayer
|
7
|