|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
twin-engine jet
|
|
gptkbp:aircraft_operated
|
experimental
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:configuration
|
twin-engine
|
|
gptkbp:country
|
gptkb:United_Kingdom
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:crew_capacity
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
experimental design
|
|
gptkbp:design_date
|
1950s
|
|
gptkbp:development
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:engine
|
gptkb:Rolls-Royce
|
|
gptkbp:engine_type
|
gptkb:turbofan_engine
RB.108
|
|
gptkbp:first_flight
|
1953
1953-06-01
|
|
gptkbp:fuel_capacity
|
2000 L
|
|
gptkbp:height
|
3.81 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.113
|
|
gptkbp:landing_distance
|
600 m
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.80 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
800 km/h
|
|
gptkbp:max_takeoff_weight
|
5000 kg
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:payload_capacity
|
1000 kg
|
|
gptkbp:primary_function
|
research and development
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:related_aircraft
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:retired
|
gptkb:1955
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_ceiling
|
12000 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:takeoff_distance
|
800 m
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:used_by
|
gptkb:Royal_Air_Force
|
|
gptkbp:wing_area
|
40 m²
|
|
gptkbp:wing_configuration
|
swept wing
|
|
gptkbp:wingspan
|
15.24 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|