|
gptkbp:instanceOf
|
experimental aircraft
|
|
gptkbp:aircraft
|
gptkb:X-29
fighter aircraft
experimental design
unconventional
|
|
gptkbp:airlines
|
expanded flight capabilities
|
|
gptkbp:avionics
|
advanced digital systems
|
|
gptkbp:built
|
2
|
|
gptkbp:cockpit
|
NASA_test_pilots
|
|
gptkbp:collaborations
|
gptkb:U.S._Air_Force
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
1
|
|
gptkbp:decommissioned
|
1992
|
|
gptkbp:design_feature
|
forward-swept wings
forward-swept wing configuration
|
|
gptkbp:engineType
|
twin-engine
|
|
gptkbp:firstFlight
|
gptkb:NASA_Dryden_Flight_Research_Center
1984
over 200
|
|
gptkbp:flowsInto
|
extensive
|
|
gptkbp:height
|
4.5 meters
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
The X-29 Experimental Aircraft
|
|
gptkbp:impact
|
aeronautical engineering
|
|
gptkbp:influenced
|
future aircraft designs
|
|
gptkbp:inspiration
|
modern stealth fighters
|
|
gptkbp:inventor
|
X-29A
|
|
gptkbp:legacy
|
pioneering aircraft technology
|
|
gptkbp:length
|
15.2 meters
|
|
gptkbp:manufacturer
|
gptkb:McDonnell_Douglas
|
|
gptkbp:maximum_speed
|
gptkb:Mach_2.4
|
|
gptkbp:maxTakeoffWeight
|
12,000 pounds
|
|
gptkbp:missions
|
enhanced maneuverability
|
|
gptkbp:notable_feature
|
variable camber wings
|
|
gptkbp:operationalHistory
|
limited but influential
|
|
gptkbp:operationalRange
|
1,000 miles
|
|
gptkbp:research_areas
|
stealth_technology
|
|
gptkbp:research_focus
|
aerodynamic efficiency
control and stability
|
|
gptkbp:retired
|
1992
|
|
gptkbp:role
|
technology demonstrator
|
|
gptkbp:secondary_mission
|
X-29B
|
|
gptkbp:session
|
advanced technologies
|
|
gptkbp:significance
|
aerodynamic research
|
|
gptkbp:speed
|
100 knots
|
|
gptkbp:succeededBy
|
60 degrees per second
|
|
gptkbp:team
|
NASA_and_McDonnell_Douglas
|
|
gptkbp:training
|
gptkb:NASA's_Advanced_Fighter_Technology_Integration
|
|
gptkbp:wingspan
|
11.6 meters
|