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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:North_American_F-100_Super_Sabre
gptkb:Hugh_E._Mc_Elroy
low-wing
experimental testbed
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gptkbp:avionics
|
analog systems
|
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gptkbp:cockpit
|
single-seat
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gptkbp:controls
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fly-by-wire
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gptkbp:crew
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gptkb:musical
|
|
gptkbp:design
|
Hughes Aircraft engineers
test variable-sweep wing
|
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gptkbp:engine
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gptkb:Pratt_&_Whitney
|
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gptkbp:engine_type
|
turbojet
J57
|
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gptkbp:features
|
swept wings
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gptkbp:first_flight
|
gptkb:1956
conducted by United States Air Force
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|
gptkbp:fuel_capacity
|
2,000 lb
|
|
gptkbp:height
|
12 ft 0 in
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|
gptkbp:historical_significance
|
pioneered variable-sweep wing technology.
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|
https://www.w3.org/2000/01/rdf-schema#label
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Hughes X-5
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gptkbp:influenced_by
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German aircraft designs
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gptkbp:invention
|
X-5-1
|
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gptkbp:is_tested_for
|
variable-sweep wing technology
|
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gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
gptkb:Hughes_XF-11
|
|
gptkbp:length
|
45 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Hughes_Aircraft_Company
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gptkbp:max_speed
|
600 mph
|
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gptkbp:number_built
|
gptkb:musical
|
|
gptkbp:retirement_year
|
gptkb:1959
|
|
gptkbp:role
|
research and development
|
|
gptkbp:roll_rate
|
5 degrees per second
|
|
gptkbp:service_ceiling
|
40,000 ft
|
|
gptkbp:significance
|
early variable-sweep wing research
|
|
gptkbp:speed
|
100 knots
|
|
gptkbp:status
|
retired
|
|
gptkbp:surface
|
elevators
ailerons
rudder
|
|
gptkbp:tail_type
|
T-tail
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gptkbp:weight
|
12,000 lb
|
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gptkbp:wing_area
|
300 sq ft
|
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gptkbp:wingspan
|
35 ft 0 in
|
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gptkbp:bfsParent
|
gptkb:Hughes_Aircraft_Company
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gptkbp:bfsLayer
|
4
|