|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
|
|
gptkbp:bfsParent
|
gptkb:Sir_Frederick_Handley_Page
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:military_officer
gptkb:John_Cunningham
aluminum
experimental
straight wing
testbed for new technologies
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:country
|
gptkb:United_Kingdom
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:date
|
gptkb:1952
|
|
gptkbp:design
|
gptkb:Sir_Frederick_Handley_Page
research in high-speed flight
|
|
gptkbp:engine
|
gptkb:musical
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:features
|
swept wings
|
|
gptkbp:first_flight
|
gptkb:battle
1953
1953-09-01
1955-06-01
|
|
gptkbp:height
|
3.2 m
|
|
gptkbp:historical_significance
|
pioneering jet aircraft design
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Handley Page H. P.110
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
10.7 m
|
|
gptkbp:manufacturer
|
gptkb:Handley_Page
|
|
gptkbp:material
|
aluminum
high aspect ratio wing
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
3,000 kg
|
|
gptkbp:number_built
|
gptkb:musical
|
|
gptkbp:power_output
|
gptkb:Rolls-Royce_Derwent
|
|
gptkbp:propulsion
|
jet propulsion
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
5°/s
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:status
|
retired
|
|
gptkbp:surface
|
elevators
ailerons
rudder
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:used_in
|
aerodynamics research
|
|
gptkbp:wing_area
|
30 m²
|
|
gptkbp:wingspan
|
12.8 m
|