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gptkbp:instance_of
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gptkb:aircraft
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|
gptkbp:air_traffic_control
|
active control system
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|
gptkbp:aircraft_configuration
|
tailless design
|
|
gptkbp:aircraft_operated
|
advanced materials
integrated systems
evaluated
influential in aerospace engineering
experimental aircraft category
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gptkbp:aircraft_type
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gptkb:fighter_aircraft
|
|
gptkbp:avionics
|
advanced avionics
|
|
gptkbp:cockpit
|
glass cockpit
|
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gptkbp:contribution
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aerodynamics and control systems
|
|
gptkbp:control_surfaces
|
elevons
|
|
gptkbp:control_system
|
fly-by-wire
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
forward-swept wings
NASA and Mc Donnell Douglas
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|
gptkbp:design_features
|
variable geometry wings
|
|
gptkbp:design_purpose
|
improve maneuverability
|
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gptkbp:engine
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gptkb:General_Electric_F404
|
|
gptkbp:financial_stability
|
improved stability characteristics
|
|
gptkbp:first_flight
|
gptkb:1984
completed
numerous
completed successfully
extensively recorded
|
|
gptkbp:flight_research
|
pioneering
|
|
gptkbp:flight_style
|
unique
expanded
|
|
gptkbp:flight_tests_conducted_by
|
NASA and USAF
|
|
gptkbp:fuselage_material
|
composite materials
|
|
gptkbp:has_authority_over
|
enhanced
|
|
gptkbp:height
|
4.3 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-29 experimental aircraft
|
|
gptkbp:impact
|
gptkb:significant
|
|
gptkbp:inspiration
|
future aircraft designs
|
|
gptkbp:is_tested_for
|
gptkb:NASA
new technologies
|
|
gptkbp:landing_distance
|
short
|
|
gptkbp:landing_gear
|
tricycle type
|
|
gptkbp:legacy
|
influenced modern aircraft design
|
|
gptkbp:length
|
15.2 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:notable_pilots
|
gptkb:NASA_test_pilots
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_history
|
limited
|
|
gptkbp:operational_use
|
gptkb:none
|
|
gptkbp:project
|
gptkb:X-29
1981 to 1992
|
|
gptkbp:research_areas
|
flight dynamics
|
|
gptkbp:research_duration
|
8 years
|
|
gptkbp:research_focus
|
aerodynamic efficiency
|
|
gptkbp:retired
|
gptkb:1992
|
|
gptkbp:role
|
technology demonstrator
|
|
gptkbp:roll_control_system
|
gptkb:advanced_technology
|
|
gptkbp:roll_rate
|
high
wing warping
|
|
gptkbp:significance
|
first forward-swept wing aircraft to fly
|
|
gptkbp:stall_speed
|
improved
|
|
gptkbp:takeoff_distance
|
short
|
|
gptkbp:used_for
|
aerodynamic research
|
|
gptkbp:weight
|
approximately 7,000 kg
|
|
gptkbp:wingspan
|
11.6 m
|
|
gptkbp:bfsParent
|
gptkb:the_James_S._Mc_Donnell_Space_Hangar
|
|
gptkbp:bfsLayer
|
5
|