|
gptkbp:instanceOf
|
experimental aircraft
|
|
gptkbp:air_traffic_control
|
adaptive
|
|
gptkbp:aircraft
|
fighter aircraft
experimental
unique
integrated
tailless
evaluated
influenced future designs
technology demonstrator
experimental configuration
swept-back
|
|
gptkbp:airlines
|
expanded
|
|
gptkbp:avionics
|
advanced
|
|
gptkbp:built
|
9 years
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:collaborations
|
gptkb:NASA_Ames_Research_Center
|
|
gptkbp:constructionMaterial
|
composite materials
|
|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
1
NASA_test_pilots
|
|
gptkbp:design_feature
|
forward-swept wings
|
|
gptkbp:educational_programs
|
gptkb:Advanced_Fighter_Technology_Integration
|
|
gptkbp:engineType
|
twin-engine
|
|
gptkbp:firstFlight
|
gptkb:Edwards_Air_Force_Base
1984
1992
extensive
successful
|
|
gptkbp:funding
|
government funded
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-29
|
|
gptkbp:inspiration
|
innovative
superior agility
|
|
gptkbp:inventor
|
2
X-29A
|
|
gptkbp:is_a_symbol_of
|
advanced technologies
|
|
gptkbp:is_governed_by
|
high
|
|
gptkbp:is_used_in
|
research and development
|
|
gptkbp:landing_gear
|
retractable
|
|
gptkbp:length
|
15.2 m
|
|
gptkbp:manufacturer
|
gptkb:McDonnell_Douglas
|
|
gptkbp:maximum_speed
|
gptkb:Mach_2.0
|
|
gptkbp:notable_feature
|
variable camber wings
|
|
gptkbp:notableWork
|
significant
|
|
gptkbp:operationalHistory
|
limited
|
|
gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:releaseYear
|
1983
|
|
gptkbp:reportsTo
|
published
|
|
gptkbp:research_focus
|
aerodynamics
|
|
gptkbp:role
|
technology demonstrator
|
|
gptkbp:services
|
enhanced
|
|
gptkbp:speed
|
improved
|
|
gptkbp:succeededBy
|
high
|
|
gptkbp:successor
|
none
|
|
gptkbp:surface
|
elevons
|
|
gptkbp:team
|
NASA_and_McDonnell_Douglas
|
|
gptkbp:tourism
|
over 200
|
|
gptkbp:weight
|
6,000 kg
|
|
gptkbp:wingspan
|
11.6 m
|