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gptkbp:instance_of
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gptkb:stealth_technology
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|
gptkbp:air_traffic_control
|
fly-by-wire
|
|
gptkbp:aircraft_configuration
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gptkb:classified_information
tailless design
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|
gptkbp:aircraft_operated
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gptkb:military_aircraft
high maneuverability
fly-by-wire system
advanced radar system
influenced future designs
18,000 kg
influenced future stealth designs
19,000 kg
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|
gptkbp:aircraft_role
|
multirole capabilities
|
|
gptkbp:aircraft_type
|
gptkb:YF-23_A
gptkb:fighter_aircraft
|
|
gptkbp:armament
|
air-to-air missiles
|
|
gptkbp:avionics
|
advanced radar system
advanced avionics system
|
|
gptkbp:awards
|
ATF design competition
ATF competition
|
|
gptkbp:cockpit
|
glass cockpit
|
|
gptkbp:combat_radius
|
1,200 km
|
|
gptkbp:competed_in
|
gptkb:YF-22
gptkb:Lockheed_YF-22
|
|
gptkbp:control_surfaces
|
canard and tail surfaces
canard and tail
|
|
gptkbp:countermeasures
|
electronic warfare systems
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:cultural_heritage
|
derived from earlier Northrop designs
|
|
gptkbp:decided_by
|
YF-22 selected for production
|
|
gptkbp:design
|
fifth generation
Northrop and Mc Donnell Douglas
|
|
gptkbp:design_features
|
advanced aerodynamics
|
|
gptkbp:design_philosophy
|
supercruise capability
stealth and supercruise
|
|
gptkbp:designated_as
|
gptkb:US_Air_Force
|
|
gptkbp:engine
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gptkb:General_Electric
|
|
gptkbp:engine_type
|
twin-engine
YF120
|
|
gptkbp:first_flight
|
gptkb:1990
numerous
extensive ground testing
numerous test flights conducted
by US Air Force
|
|
gptkbp:fuel_capacity
|
9,000 liters
|
|
gptkbp:fuselage_material
|
composite materials
|
|
gptkbp:has_programs
|
gptkb:Advanced_Tactical_Fighter_(ATF)_program
|
|
gptkbp:height
|
4.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
YF-23
|
|
gptkbp:invention
|
2
|
|
gptkbp:is_part_of
|
gptkb:Advanced_Tactical_Fighter_(ATF)_program
|
|
gptkbp:is_targeted_at
|
infrared search and track
|
|
gptkbp:landing_gear
|
retractable
retractable landing gear
|
|
gptkbp:length
|
20.2 m
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Grumman
|
|
gptkbp:max_speed
|
Mach 2.0
|
|
gptkbp:nickname
|
gptkb:Black_Widow_II
|
|
gptkbp:notable_pilots
|
one pilot
multiple test pilots involved
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_range
|
1,500 km
2,500 km
|
|
gptkbp:production_status
|
not produced
|
|
gptkbp:project
|
prototype phase
|
|
gptkbp:project_cancellation
|
canceled after ATF selection
|
|
gptkbp:propulsion
|
greater than 1
22,000 lbf per engine
|
|
gptkbp:radar
|
gptkb:radar_system
low radar cross-section
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:release_date
|
gptkb:1990
|
|
gptkbp:result
|
not selected for production
|
|
gptkbp:role
|
gptkb:stealth_technology
air superiority
multirole fighter
|
|
gptkbp:roll_rate
|
high roll rate
|
|
gptkbp:seating_capacity
|
gptkb:Martin-Baker_Mk.16
|
|
gptkbp:service_ceiling
|
15,240 m
|
|
gptkbp:status
|
retired
|
|
gptkbp:stealth_features
|
yes
low radar cross-section
blended wing body
minimized heat signature
shaped surfaces
|
|
gptkbp:stealth_materials
|
radar-absorbent materials
|
|
gptkbp:wing_configuration
|
variable-sweep wing
|
|
gptkbp:wingspan
|
13.2 m
|
|
gptkbp:bfsParent
|
gptkb:Advanced_Tactical_Fighter_(ATF)_program
gptkb:Edwards_Air_Force_Base
gptkb:Skunk_Works
|
|
gptkbp:bfsLayer
|
5
|