|
gptkbp:instance_of
|
gptkb:fighter_aircraft
|
|
gptkbp:aircraft_configuration
|
gptkb:radar_system
gptkb:safety_equipment
gptkb:gasoline
gptkb:furniture
twin-engine
control surfaces
horizontal stabilizer
vertical stabilizer
single-seat
high wing
low wing
tailplane
tail design
wing structure
engine nacelle
fuselage design
wing loading
canard design
cockpit design
canopy design
drop tanks
nose design
wingtip missiles
|
|
gptkbp:aircraft_type
|
multirole fighter
|
|
gptkbp:armament
|
gptkb:cannon
air-to-air missiles
air-to-ground missiles
|
|
gptkbp:avionics
|
digital fly-by-wire
|
|
gptkbp:combat_radius
|
2,280 km
|
|
gptkbp:combat_role
|
gptkb:training
|
|
gptkbp:crew
|
gptkb:1
|
|
gptkbp:design
|
single-engine
|
|
gptkbp:design_date
|
1972-1974
|
|
gptkbp:design_team_leader
|
gptkb:Harry_Hillaker
|
|
gptkbp:developed_by
|
gptkb:General_Dynamics_F-16_Fighting_Falcon
|
|
gptkbp:engine_type
|
gptkb:Pratt_&_Whitney_F100
turbofan
|
|
gptkbp:exported_to
|
gptkb:various_countries
|
|
gptkbp:first_flight
|
gptkb:1974
January 20, 1974
|
|
gptkbp:has_programs
|
Lightweight Fighter Program
|
|
gptkbp:height
|
4.88 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
YF-16
|
|
gptkbp:invention
|
gptkb:YF-16_A
|
|
gptkbp:is_tested_for
|
avionics systems
YF-16 program
|
|
gptkbp:length
|
14.8 m
|
|
gptkbp:manufacturer
|
gptkb:General_Dynamics
|
|
gptkbp:max_speed
|
2,124 km/h
|
|
gptkbp:notable_features
|
advanced avionics
lightweight design
high maneuverability
|
|
gptkbp:number_built
|
2
|
|
gptkbp:operational_history
|
limited
|
|
gptkbp:propulsion
|
1.1:1
|
|
gptkbp:related_aircraft
|
gptkb:F-16_family
|
|
gptkbp:role
|
air superiority
|
|
gptkbp:second_prototype
|
gptkb:YF-16_B
|
|
gptkbp:service_ceiling
|
15,240 m
|
|
gptkbp:stealth_features
|
limited
|
|
gptkbp:successor
|
gptkb:F-16_Fighting_Falcon
|
|
gptkbp:used_by
|
gptkb:United_States_Air_Force
|
|
gptkbp:wing_configuration
|
delta wing
|
|
gptkbp:wingspan
|
9.96 m
|
|
gptkbp:bfsParent
|
gptkb:F-16_Fighting_Falcon
|
|
gptkbp:bfsLayer
|
4
|