gptkbp:instance_of
|
gptkb:aircraft
|
gptkbp:air_traffic_control
|
manual control
|
gptkbp:aircraft_configuration
|
delta wing
|
gptkbp:aircraft_operated
|
experimental aircraft category
|
gptkbp:aircraft_role
|
research and development
|
gptkbp:armament
|
gptkb:none
|
gptkbp:ceiling
|
15,000 m
|
gptkbp:control_surfaces
|
elevons
|
gptkbp:country
|
gptkb:United_Kingdom
|
gptkbp:crew
|
gptkb:1
|
gptkbp:design
|
tailless design
Handley Page engineers
|
gptkbp:design_date
|
1940s-1950s
|
gptkbp:design_features
|
high aspect ratio wings
|
gptkbp:development
|
H. P.88
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Avon
turbojet
|
gptkbp:first_flight
|
gptkb:Boscombe_Down
1953
1954-01-01
1953-07-01
conducted by Royal Aircraft Establishment
|
gptkbp:fuel_capacity
|
1,500 liters
|
gptkbp:fuselage_material
|
gptkb:metal
|
gptkbp:height
|
3.96 m
|
gptkbp:historical_context
|
Cold War era aviation research
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.91
|
gptkbp:influenced_by
|
German wartime designs
|
gptkbp:landing_distance
|
400 m
|
gptkbp:landing_gear
|
retractable
|
gptkbp:length
|
12.80 m
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
gptkbp:max_speed
|
1,000 km/h
|
gptkbp:max_takeoff_weight
|
3,175 kg
|
gptkbp:notable_pilots
|
gptkb:John_Cunningham
|
gptkbp:number_built
|
gptkb:1
|
gptkbp:number_of_engines
|
gptkb:1
|
gptkbp:predecessor
|
gptkb:Handley_Page_H._P.88
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
gptkbp:propulsion
|
jet propulsion
|
gptkbp:related_aircraft
|
gptkb:Handley_Page_Victor
gptkb:Handley_Page_Halifax
gptkb:Handley_Page_Hastings
|
gptkbp:role
|
gptkb:aircraft
|
gptkbp:roll_rate
|
10°/s
|
gptkbp:significance
|
research into delta wing configurations
|
gptkbp:stall_speed
|
120 km/h
|
gptkbp:status
|
retired
|
gptkbp:successor
|
gptkb:none
|
gptkbp:takeoff_distance
|
300 m
|
gptkbp:type
|
gptkb:aircraft
|
gptkbp:wing_area
|
40 m²
|
gptkbp:wingspan
|
15.24 m
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
gptkb:John_Handley_Page
|
gptkbp:bfsLayer
|
6
|