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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:aircraft_altitude
|
30,000 ft
|
|
gptkbp:aircraft_configuration
|
canard
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|
gptkbp:aircraft_design_feature
|
hover capability
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
5,000 lb
basic instrumentation
funded by US government
paved the way for future VTOL aircraft.
|
|
gptkbp:aircraft_role
|
research and development
|
|
gptkbp:aircraft_tail
|
T-tail
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|
gptkbp:aircraft_thrust
|
5,000 lbf
|
|
gptkbp:aircraft_wings
|
delta wings
|
|
gptkbp:ceiling
|
30,000 ft
|
|
gptkbp:cockpit
|
single-seat
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
gptkb:jet_engine
Hughes Aircraft engineers
|
|
gptkbp:design_date
|
1953
|
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gptkbp:first_flight
|
gptkb:1956
completed in 1959
|
|
gptkbp:fuel_capacity
|
1,000 lb
|
|
gptkbp:height
|
8 ft 0 in
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hughes X-13
|
|
gptkbp:influenced
|
later VTOL designs
|
|
gptkbp:is_tested_for
|
gptkb:US_Navy
|
|
gptkbp:landing_distance
|
60 mph
vertical landing
|
|
gptkbp:landing_gear
|
retractable
|
|
gptkbp:length
|
30 ft 0 in
|
|
gptkbp:manufacturer
|
gptkb:Hughes_Aircraft_Company
|
|
gptkbp:max_speed
|
300 mph
|
|
gptkbp:notable_pilots
|
gptkb:Robert_C._Mc_Donnell
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_use
|
gptkb:none
|
|
gptkbp:power_source
|
gptkb:J65_turbojet_engine
|
|
gptkbp:range
|
500 miles
|
|
gptkbp:release_date
|
gptkb:1955
|
|
gptkbp:retirement_year
|
gptkb:1960
|
|
gptkbp:role
|
vertical takeoff and landing (VTOL) aircraft
|
|
gptkbp:significance
|
first jet VTOL aircraft
|
|
gptkbp:status
|
retired
|
|
gptkbp:takeoff_distance
|
70 mph
vertical takeoff
|
|
gptkbp:type
|
gptkb:fighter_aircraft
|
|
gptkbp:wingspan
|
30 ft 0 in
|
|
gptkbp:bfsParent
|
gptkb:Hughes_Aircraft_Company
|
|
gptkbp:bfsLayer
|
5
|