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gptkbp:instance_of
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gptkb:aircraft
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gptkbp:bfsLayer
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6
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gptkbp:bfsParent
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gptkb:Northrop_YF-23_Black_Widow_II
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:YF-23
gptkb:YF-23_A
gptkb:YF-23_B
high maneuverability
delta wing
flying wing
fly-by-wire system
air superiority fighter
tailless design
29,000 lb
part of ATF program
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gptkbp:armament
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air-to-air missiles
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gptkbp:avionics
|
advanced avionics system
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gptkbp:awards
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gptkb:Lockheed_YF-22
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gptkbp:cockpit
|
glass cockpit
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|
gptkbp:combat_radius
|
1,200 miles
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gptkbp:design
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gptkb:Northrop_Grumman
gptkb:Lockheed_Martin_F-22_Raptor
stealth and agility
low observable technology
Northrop design team
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|
gptkbp:developed_by
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gptkb:Northrop_YF-23_prototype
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gptkbp:engine
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gptkb:General_Electric
|
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gptkbp:engine_type
|
gptkb:F119-PW-100
twin-engine
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|
gptkbp:features
|
advanced radar system
supercruise capability
|
|
gptkbp:first_flight
|
gptkb:1990
extensive test flights conducted
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|
gptkbp:fuel_capacity
|
12,000 lb
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gptkbp:height
|
4.57 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Northrop YF-23 family
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gptkbp:is_used_by
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gptkb:aircraft
|
|
gptkbp:landing_gear
|
retractable landing gear
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|
gptkbp:legacy
|
influenced future stealth designs
|
|
gptkbp:length
|
20.2 m
|
|
gptkbp:manufacturer
|
gptkb:Northrop_Corporation
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|
gptkbp:material
|
aluminum and titanium
|
|
gptkbp:max_speed
|
Mach 2.0
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|
gptkbp:nickname
|
gptkb:Black_Widow_II
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_area
|
not operationally used
|
|
gptkbp:project
|
gptkb:1996
|
|
gptkbp:propulsion
|
1.1
|
|
gptkbp:role
|
gptkb:aircraft
gptkb:Advanced_Tactical_Fighter_program
|
|
gptkbp:roll_rate
|
30 degrees per second
|
|
gptkbp:service_ceiling
|
50,000 ft
|
|
gptkbp:stealth_features
|
composite materials
low radar cross-section
multi-spectral stealth
|
|
gptkbp:successor
|
gptkb:F-22_Raptor
|
|
gptkbp:surface
|
canard surfaces
|
|
gptkbp:wingspan
|
14.63 m
|