|
gptkbp:instance_of
|
gptkb:drones
|
|
gptkbp:aircraft_role
|
gptkb:drones
|
|
gptkbp:aircraft_type
|
gptkb:unmanned_aerial_vehicle
|
|
gptkbp:ceiling
|
15,000 meters
|
|
gptkbp:control_system
|
gptkb:remote_control
radio control
|
|
gptkbp:country_of_origin
|
gptkb:United_States
|
|
gptkbp:crew
|
unmanned
|
|
gptkbp:decommissioned
|
gptkb:1960
|
|
gptkbp:design
|
Hughes Aircraft engineers
|
|
gptkbp:design_date
|
gptkb:1955
|
|
gptkbp:design_features
|
high speed
|
|
gptkbp:design_purpose
|
testing missile systems
|
|
gptkbp:development
|
gptkb:Hughes_Aircraft_Company
1955-1956
|
|
gptkbp:engine
|
gptkb:Pratt_&_Whitney
|
|
gptkbp:engine_type
|
turbojet
|
|
gptkbp:first_flight
|
gptkb:1956
gptkb:1960
successful
conducted by US Air Force
|
|
gptkbp:fuel_type
|
kerosene
|
|
gptkbp:has_units
|
approximately 30
|
|
gptkbp:historical_context
|
Cold War era technology
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hughes X-10
|
|
gptkbp:influenced_by
|
previous drone designs
|
|
gptkbp:inspiration
|
modern UAV designs
|
|
gptkbp:launch_window
|
air launch
|
|
gptkbp:legacy
|
paved the way for future UAVs
|
|
gptkbp:length
|
8.5 meters
|
|
gptkbp:manufacturer
|
gptkb:Hughes_Aircraft_Company
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:notable_case
|
none reported
|
|
gptkbp:operational_status
|
retired
|
|
gptkbp:operational_use
|
gptkb:military_training
|
|
gptkbp:original_purpose
|
target practice for missiles
|
|
gptkbp:primary_use
|
target practice
|
|
gptkbp:project
|
Drones in military applications
|
|
gptkbp:range
|
1,500 km
|
|
gptkbp:retired
|
gptkb:1960
|
|
gptkbp:retirement
|
obsolescence
|
|
gptkbp:role
|
gptkb:drones
|
|
gptkbp:service_entry
|
gptkb:1956
|
|
gptkbp:significance
|
early drone technology
|
|
gptkbp:successor
|
Aqua-1
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:weight
|
3,600 kg
|
|
gptkbp:wing_configuration
|
straight wings
|
|
gptkbp:wingspan
|
8.2 meters
|
|
gptkbp:bfsParent
|
gptkb:Hughes_Aircraft_Company
|
|
gptkbp:bfsLayer
|
5
|