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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
|
3
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gptkbp:bfsParent
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gptkb:mythological_figure
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Gordon_Fullerton
1 hour 30 minutes
tailless configuration
active control system
experimental aircraft category
swept wing design
influenced future aircraft designs.
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|
gptkbp:avionics
|
digital
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|
gptkbp:controls
|
fly-by-wire
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:date
|
gptkb:1980s
|
|
gptkbp:design
|
Hercules Aerospace and NASA
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|
gptkbp:engine
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gptkb:General_Electric
|
|
gptkbp:engine_type
|
gptkb:F404
twin-engine
|
|
gptkbp:features
|
forward-swept wings
|
|
gptkbp:first_flight
|
gptkb:1984
gptkb:Edwards_Air_Force_Base
50
expanded flight envelope
agile flight characteristics
|
|
gptkbp:has_authority_over
|
high control authority
|
|
gptkbp:has_programs
|
gptkb:Advanced_Tactical_Fighter
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Hercules X-29
|
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gptkbp:influence
|
modern fighter aircraft design
|
|
gptkbp:invention
|
2
|
|
gptkbp:is_tested_for
|
gptkb:NASA's_Advanced_Fighter_Technology_Integration
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
15.2 m
|
|
gptkbp:manufacturer
|
gptkb:Hercules_Aerospace
|
|
gptkbp:material
|
composite materials
|
|
gptkbp:max_speed
|
1,000 km/h
|
|
gptkbp:max_takeoff_weight
|
8,000 kg
|
|
gptkbp:notable_feature
|
variable camber wings
|
|
gptkbp:research
|
advanced flight control systems
|
|
gptkbp:research_areas
|
gptkb:aircraft
gptkb:NASA
|
|
gptkbp:research_focus
|
aerodynamics
|
|
gptkbp:retirement_year
|
gptkb:1992
|
|
gptkbp:role
|
technology demonstrator
|
|
gptkbp:roll_rate
|
wing warping
60 degrees per second
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:significance
|
first aircraft with forward-swept wings to fly
|
|
gptkbp:successor
|
gptkb:Joint_Strike_Fighter
|
|
gptkbp:surface
|
elevons
|
|
gptkbp:wingspan
|
11.6 m
|