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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_operated
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gptkb:aircraft
experimental
adaptive control systems
forward-swept wing
two prototypes built.
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gptkbp:avionics
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modern digital systems
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gptkbp:cockpit
|
single-seat
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|
gptkbp:collaborations
|
NASA and military
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gptkbp:controls
|
fly-by-wire
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gptkbp:crew
|
one
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gptkbp:design
|
NASA and Mc Donnell Douglas
forward-swept wing aircraft
test forward-swept wing technology
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gptkbp:engine_type
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gptkb:General_Electric_F404
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gptkbp:features
|
low drag characteristics
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|
gptkbp:first_flight
|
gptkb:1984
gptkb:NASA_Dryden_Flight_Research_Center
over 200
aerospace engineering
expanded
December 14, 1984
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gptkbp:has_programs
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gptkb:Advanced_Tactical_Fighter
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|
https://www.w3.org/2000/01/rdf-schema#label
|
X-29 Forward Swept Wing
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gptkbp:influence
|
future aircraft designs
|
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gptkbp:invention
|
two
|
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gptkbp:is_tested_for
|
extensive
advanced flight control systems
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:legacy
|
influenced modern fighter jets
|
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gptkbp:length
|
15.2 m
|
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gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
composite materials
|
|
gptkbp:max_speed
|
Mach 2.5
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|
gptkbp:notable_feature
|
variable camber wings
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|
gptkbp:operational_history
|
limited
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gptkbp:origin
|
gptkb:United_States
|
|
gptkbp:performance
|
aerodynamic efficiency
|
|
gptkbp:research_areas
|
flight dynamics
|
|
gptkbp:research_focus
|
aerodynamics
|
|
gptkbp:retirement_year
|
gptkb:1992
|
|
gptkbp:role
|
technology demonstrator
|
|
gptkbp:roll_rate
|
high
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gptkbp:significance
|
demonstrated benefits of forward-swept wings
|
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gptkbp:speed
|
improved
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gptkbp:successor
|
gptkb:none
|
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gptkbp:surface
|
elevons
|
|
gptkbp:weight
|
6,000 kg
|
|
gptkbp:wingspan
|
11.6 m
|
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gptkbp:bfsParent
|
gptkb:Northrop
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gptkbp:bfsLayer
|
5
|