|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:air_traffic_control
|
fly-by-wire
|
|
gptkbp:aircraft_operated
|
experimental drone
|
|
gptkbp:aircraft_role
|
gptkb:drones
|
|
gptkbp:aircraft_type
|
gptkb:unmanned_aerial_vehicle
|
|
gptkbp:ceiling
|
15,000 meters
|
|
gptkbp:control_system
|
gptkb:remote_control
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew
|
gptkb:none
|
|
gptkbp:decommissioned
|
gptkb:1956
|
|
gptkbp:design
|
gptkb:Howard_Hughes
jet-powered
|
|
gptkbp:design_date
|
gptkb:1949
|
|
gptkbp:design_purpose
|
research and development
|
|
gptkbp:development
|
1949-1951
|
|
gptkbp:engine_type
|
turbojet
|
|
gptkbp:first_flight
|
1951
completed in 1955
conducted at Muroc Air Force Base
|
|
gptkbp:historical_context
|
Cold War era
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hughes X-6
|
|
gptkbp:influenced
|
military drone programs
|
|
gptkbp:influenced_by
|
gptkb:Hughes_D-1
|
|
gptkbp:inspired
|
future drone designs
|
|
gptkbp:is_influenced_by
|
UAV technology
|
|
gptkbp:is_tested_for
|
1950s
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
pioneering UAV technology
|
|
gptkbp:length
|
8.53 meters
|
|
gptkbp:manufacturer
|
gptkb:Hughes_Aircraft_Company
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:notable_feature
|
high speed
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operated_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:operational_use
|
gptkb:military
|
|
gptkbp:related_aircraft
|
gptkb:Hughes_X-4
|
|
gptkbp:retired
|
gptkb:1956
|
|
gptkbp:retirement
|
obsolescence
|
|
gptkbp:role
|
gptkb:drones
|
|
gptkbp:service
|
1951-1956
|
|
gptkbp:significance
|
early UAV development
|
|
gptkbp:successor
|
gptkb:Hughes_D-2
|
|
gptkbp:used_for
|
target practice
|
|
gptkbp:used_in
|
gptkb:military_exercises
|
|
gptkbp:weight
|
3,600 kg
|
|
gptkbp:wing_configuration
|
straight wings
|
|
gptkbp:wingspan
|
15.24 meters
|
|
gptkbp:bfsParent
|
gptkb:Hughes_Aircraft_Company
|
|
gptkbp:bfsLayer
|
5
|