|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:unmanned_aerial_vehicle
up to 100,000 feet
|
|
gptkbp:analysis
|
post-flight analysis
|
|
gptkbp:collaboration
|
gptkb:NASA
|
|
gptkbp:collaborations
|
gptkb:Department_of_Defense
|
|
gptkbp:collection
|
gptkb:Telehealth_Services
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:control_system
|
gptkb:remote_control
fly-by-wire system
|
|
gptkbp:data_usage
|
military applications
|
|
gptkbp:design
|
gptkb:Lockheed_Skunk_Works
aerodynamic shape
|
|
gptkbp:design_philosophy
|
stealth and speed
|
|
gptkbp:development
|
1940s to 1950s
|
|
gptkbp:engine_type
|
gptkb:Team_Rocket
|
|
gptkbp:first_flight
|
1951
completed in 1956
conducted at Edwards Air Force Base
|
|
gptkbp:flight_style
|
high maneuverability
|
|
gptkbp:fuel_type
|
liquid propellant
|
|
gptkbp:funding
|
gptkb:United_States_Air_Force
|
|
gptkbp:fuselage_material
|
aluminum
|
|
gptkbp:guidance_system
|
inertial navigation
|
|
gptkbp:has_programs
|
gptkb:Dyna-Soar
|
|
gptkbp:historical_context
|
Cold War era research
|
|
gptkbp:historical_significance
|
first drone to reach hypersonic speeds
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Lockheed X-7
|
|
gptkbp:impact
|
aerospace engineering
|
|
gptkbp:influence
|
future space vehicles
|
|
gptkbp:inspiration
|
future UAV designs
|
|
gptkbp:is_tested_for
|
gptkb:X-7_program
completed in 1956
valuable data for future designs
|
|
gptkbp:launch_platform
|
gptkb:bomber
|
|
gptkbp:launch_window
|
air launch
|
|
gptkbp:legacy
|
pioneering hypersonic technology
|
|
gptkbp:length
|
8.2 meters
|
|
gptkbp:manufacturer
|
gptkb:Lockheed_Corporation
|
|
gptkbp:max_speed
|
Mach 3.2
|
|
gptkbp:notable_feature
|
high-speed performance
|
|
gptkbp:notable_pilots
|
not applicable
|
|
gptkbp:number_built
|
gptkb:6
|
|
gptkbp:operational_challenges
|
high-speed stability
|
|
gptkbp:operational_range
|
limited
|
|
gptkbp:operational_use
|
gptkb:ground
military research
|
|
gptkbp:project
|
5 years
|
|
gptkbp:purpose
|
research and development
|
|
gptkbp:research_areas
|
aerodynamics
|
|
gptkbp:retirement
|
completion of objectives
|
|
gptkbp:role
|
testbed for hypersonic flight
|
|
gptkbp:significance
|
early hypersonic research
|
|
gptkbp:significant_event
|
first successful flight in 1953
|
|
gptkbp:status
|
retired
|
|
gptkbp:successor
|
gptkb:X-15
|
|
gptkbp:type
|
gptkb:drones
|
|
gptkbp:weight
|
3,000 pounds
|
|
gptkbp:wingspan
|
8.5 meters
|
|
gptkbp:bfsParent
|
gptkb:Hughes_X-2
|
|
gptkbp:bfsLayer
|
6
|