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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
multiple
adaptive
experimental
delta wing
approximately 7,000 kg
advanced maneuverability research
|
|
gptkbp:avionics
|
digital fly-by-wire system
|
|
gptkbp:controls
|
fly-by-wire
thrust vectoring
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:design
|
NASA and Mc Donnell Douglas
demonstrate advanced maneuverability
|
|
gptkbp:developed_by
|
gptkb:aircraft
|
|
gptkbp:engine_type
|
twin-engine
|
|
gptkbp:exhibited_at
|
gptkb:battle
|
|
gptkbp:first_flight
|
gptkb:1990
numerous
unique
expanded
|
|
gptkbp:has_authority_over
|
high angle of attack
|
|
gptkbp:height
|
4.57 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
X-31 Enhanced Fighter Maneuverability
|
|
gptkbp:influenced
|
future fighter designs
|
|
gptkbp:is_capable_of
|
high agility
|
|
gptkbp:is_tested_for
|
1990-1995
|
|
gptkbp:length
|
15.24 m
|
|
gptkbp:manufacturer
|
gptkb:Mc_Donnell_Douglas
|
|
gptkbp:material
|
composite materials
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_area
|
gptkb:none
|
|
gptkbp:project
|
5 years
|
|
gptkbp:research_focus
|
supermaneuverability
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
high
thrust vectoring
demonstrated
|
|
gptkbp:significance
|
advanced flight control technology
|
|
gptkbp:speed
|
improved
|
|
gptkbp:stealth_features
|
limited radar cross-section
|
|
gptkbp:strikeouts
|
canard surfaces
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:surface
|
canard wings
|
|
gptkbp:used_in
|
aerobatic demonstrations
|
|
gptkbp:wingspan
|
14.63 m
|
|
gptkbp:bfsParent
|
gptkb:Northrop
|
|
gptkbp:bfsLayer
|
5
|