gptkbp:instanceOf
|
experimental aircraft
|
gptkbp:aircraft
|
fighter aircraft
experimental
|
gptkbp:airlines
|
expanded
|
gptkbp:avionics
|
digital
|
gptkbp:built
|
2
|
gptkbp:campusFacilities
|
gptkb:NASA_Dryden_Flight_Research_Center
|
gptkbp:collaborations
|
gptkb:U.S._Air_Force
|
gptkbp:constructionMaterial
|
composite materials
|
gptkbp:controls
|
fly-by-wire
|
gptkbp:crew
|
gptkb:Gordon_Fullerton
1
|
gptkbp:decommissioned
|
1995
|
gptkbp:design
|
variable-sweep wing
|
gptkbp:design_feature
|
highly maneuverable
|
gptkbp:engineType
|
twin-engine
|
gptkbp:exhibits
|
yes
high angle of attack maneuvers
|
gptkbp:financial_aid
|
thrust vectoring
|
gptkbp:firstFlight
|
1990
over 100
successful
|
gptkbp:fuel_capacity
|
2,500 liters
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-31
|
gptkbp:influenced
|
gptkb:F-22_Raptor
|
gptkbp:is_a_symbol_of
|
thrust vectoring
|
gptkbp:is_used_in
|
aerodynamic research
NASA_research_programs
|
gptkbp:landing_gear
|
tricycle type
|
gptkbp:legacy
|
influenced future aircraft designs
|
gptkbp:length
|
15.2 meters
|
gptkbp:manufacturer
|
NASA
|
gptkbp:maximum_speed
|
Mach_1.5
|
gptkbp:maxRange
|
15,000 meters
|
gptkbp:missions
|
advanced algorithms
|
gptkbp:notable_feature
|
canard_configuration
|
gptkbp:notableEvent
|
gptkb:Advanced_Fighter_Technology_Integration
|
gptkbp:number_of_stages
|
completed
|
gptkbp:operational_status
|
none
|
gptkbp:operationalRange
|
1,500 kilometers
|
gptkbp:origin
|
gptkb:United_States
|
gptkbp:research_areas
|
aerodynamics
|
gptkbp:research_focus
|
stealth_technology
|
gptkbp:retired
|
1995
|
gptkbp:role
|
demonstrator for advanced technologies
|
gptkbp:significance
|
pioneered new flight technologies
|
gptkbp:speed
|
120 knots
|
gptkbp:succeededBy
|
60 degrees per second
|
gptkbp:successor
|
gptkb:X-32
|
gptkbp:surface
|
elevons
|
gptkbp:surrounding_area
|
30 square meters
|
gptkbp:team
|
gptkb:McDonnell_Douglas
|
gptkbp:weight
|
6,000 kg
|
gptkbp:wingspan
|
9.1 meters
|