|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_configuration
|
high-wing
|
|
gptkbp:aircraft_operated
|
experimental
|
|
gptkbp:aircraft_role
|
research and development
|
|
gptkbp:aircraft_type
|
experimental jet
|
|
gptkbp:ceiling
|
12,000 m
|
|
gptkbp:configuration
|
twin-engine
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
Handley Page design team
|
|
gptkbp:design_date
|
1940s to 1950s
|
|
gptkbp:design_features
|
swept wings
|
|
gptkbp:development
|
post-war aviation technology
|
|
gptkbp:engine
|
gptkb:Rolls-Royce
|
|
gptkbp:engine_type
|
turbofan
RB.145
|
|
gptkbp:first_flight
|
1950
conducted by British government
|
|
gptkbp:fuel_capacity
|
10,000 liters
|
|
gptkbp:fuselage_material
|
aluminum
|
|
gptkbp:historical_significance
|
contributed to jet technology advancements
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.99
|
|
gptkbp:influenced_by
|
H. P.88
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
25.6 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
800 km/h
|
|
gptkbp:max_takeoff_weight
|
30,000 kg
|
|
gptkbp:notable_features
|
variable-sweep wings
|
|
gptkbp:notable_pilots
|
gptkb:John_Doe
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:operational_history
|
used for military research
|
|
gptkbp:passenger_capacity
|
gptkb:0
|
|
gptkbp:performance
|
high speed and altitude
|
|
gptkbp:predecessor
|
gptkb:Handley_Page_H._P.88
|
|
gptkbp:production_status
|
limited production
|
|
gptkbp:range
|
2,000 km
|
|
gptkbp:related_aircraft
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:retirement
|
gptkb:1955
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:service_entry
|
1951
|
|
gptkbp:successor
|
gptkb:Handley_Page_Victor
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:used_in
|
gptkb:British_Air_Force
|
|
gptkbp:wing_area
|
150 m²
|
|
gptkbp:wingspan
|
30.5 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
gptkb:John_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|