Statements (90)
| Predicate | Object |
|---|---|
| gptkbp:instance_of |
gptkb:aircraft
|
| gptkbp:bfsLayer |
4
|
| gptkbp:bfsParent |
gptkb:Edwards_Air_Force_Base
gptkb:Skunk_Works |
| gptkbp:aircraft_operated |
gptkb:aircraft
gptkb:YF-23_A gptkb:market fly-by-wire high maneuverability variable-sweep wing fly-by-wire system advanced radar system influenced future designs multirole capabilities 18,000 kg influenced future stealth designs tailless design one pilot 19,000 kg multiple test pilots involved |
| 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:countermeasures |
electronic warfare systems
|
| gptkbp:crew |
gptkb:musical
|
| gptkbp:cultural_heritage |
derived from earlier Northrop designs
|
| gptkbp:decided_by |
YF-22 selected for production
|
| gptkbp:design |
fifth generation
supercruise capability stealth and supercruise Northrop and Mc Donnell Douglas |
| gptkbp:designated_as |
gptkb:US_Air_Force
|
| gptkbp:engine |
gptkb:General_Electric
|
| gptkbp:engine_type |
twin-engine
Y F120 |
| gptkbp:features |
advanced aerodynamics
|
| gptkbp:first_flight |
gptkb:1990
numerous extensive ground testing numerous test flights conducted by US Air Force |
| gptkbp:fuel_capacity |
9,000 liters
|
| 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_aimed_at |
infrared search and track
|
| gptkbp:is_part_of |
gptkb:Advanced_Tactical_Fighter_(ATF)_program
|
| gptkbp:landing_gear |
retractable
retractable landing gear |
| gptkbp:length |
20.2 m
|
| gptkbp:manufacturer |
gptkb:Northrop_Grumman
|
| gptkbp:material |
composite materials
|
| gptkbp:max_speed |
Mach 2.0
|
| gptkbp:nickname |
gptkb:Black_Widow_II
|
| gptkbp:number_built |
2
|
| gptkbp:operational_range |
1,500 km
2,500 km |
| gptkbp:participated_in |
gptkb:YF-22
gptkb:Lockheed_YF-22 |
| gptkbp:produced_by |
not produced
|
| gptkbp:project |
prototype phase
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:aircraft
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 |
gptkb:battle
low radar cross-section blended wing body minimized heat signature radar-absorbent materials shaped surfaces |
| gptkbp:surface |
canard and tail surfaces
canard and tail |
| gptkbp:wingspan |
13.2 m
|