|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
|
|
gptkbp:aircraft_role
|
civil transport
|
|
gptkbp:aircraft_type
|
fixed-wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:cargo_capacity
|
10000 kg
|
|
gptkbp:climb_rate
|
5 m/s
|
|
gptkbp:country_of_origin
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:1
2
|
|
gptkbp:design
|
gptkb:Geoffrey_Handley_Page
gptkb:prototype
Handley Page design team
|
|
gptkbp:design_date
|
1948
|
|
gptkbp:engine
|
gptkb:Rolls-Royce
|
|
gptkbp:engine_power
|
2000 hp
|
|
gptkbp:engine_type
|
gptkb:Rolls-Royce_Dart
turboprop
|
|
gptkbp:first_flight
|
gptkb:1960
1950
|
|
gptkbp:fuel_capacity
|
5000 L
|
|
gptkbp:fuselage_material
|
30.0 m
|
|
gptkbp:height
|
8.0 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.90
|
|
gptkbp:landing_distance
|
120 km/h
|
|
gptkbp:landing_gear
|
gptkb:Cycling
|
|
gptkbp:length
|
30.0 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:max_speed
|
500 km/h
|
|
gptkbp:max_takeoff_weight
|
20000 kg
25000 kg
|
|
gptkbp:number_built
|
gptkb:1
|
|
gptkbp:number_of_engines
|
2
|
|
gptkbp:passenger_capacity
|
50
|
|
gptkbp:payload_capacity
|
10000 kg
|
|
gptkbp:primary_user
|
gptkb:Royal_Air_Force
|
|
gptkbp:production_years
|
1950
|
|
gptkbp:propeller
|
gptkb:4
|
|
gptkbp:range
|
2000 km
|
|
gptkbp:retirement
|
gptkb:1960
|
|
gptkbp:role
|
gptkb:transport_aircraft
|
|
gptkbp:service_ceiling
|
8000 m
|
|
gptkbp:service_entry
|
1951
|
|
gptkbp:status
|
retired
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:takeoff_distance
|
150 km/h
|
|
gptkbp:variant
|
gptkb:Handley_Page_H._P.90_A
|
|
gptkbp:wing_area
|
200 m²
|
|
gptkbp:wing_configuration
|
high-wing
cantilever wing
|
|
gptkbp:wingspan
|
40.0 m
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
gptkb:John_Handley_Page
|
|
gptkbp:bfsLayer
|
6
|