|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aspect_ratio
|
5:1
|
|
gptkbp:avionics
|
modern avionics
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:color_scheme
|
military camouflage
|
|
gptkbp:control_surfaces
|
elevators
ailerons
rudder
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:design_date
|
gptkb:1952
|
|
gptkbp:design_features
|
swept wings
|
|
gptkbp:design_purpose
|
research and development
|
|
gptkbp:engine
|
gptkb:Rolls-Royce_Avon
|
|
gptkbp:engine_type
|
turbofan
|
|
gptkbp:first_flight
|
gptkb:1954
1954-07-01
|
|
gptkbp:fuel_capacity
|
1,000 liters
|
|
gptkbp:fuselage_material
|
high-wing
|
|
gptkbp:height
|
3.81 m
|
|
gptkbp:historical_significance
|
early jet technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.94
|
|
gptkbp:influenced_by
|
gptkb:de_Havilland_Comet
|
|
gptkbp:landing_distance
|
120 km/h
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
12.80 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
4,000 kg
3,600 kg
|
|
gptkbp:navigation_system
|
inertial navigation
|
|
gptkbp:notable_pilots
|
gptkb:John_Derry
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
gptkb:1
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:propulsion
|
jet propulsion
50 k N
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:stall_speed
|
80 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:Handley_Page_H._P.115
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:type
|
gptkb:aircraft
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wing_configuration
|
straight wing
|
|
gptkbp:wingspan
|
15.24 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
gptkb:John_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|