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gptkbp:instance_of
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gptkb:fighter_aircraft
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gptkbp:aircraft_type
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single-engine
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gptkbp:armament
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2 × 12.7 mm UBS machine guns
1 × 23 mm Nudelman-Suranov NS-23 cannon
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gptkbp:ceiling
|
12,000 m
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gptkbp:climb_rate
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20 m/s
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gptkbp:cockpit
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enclosed cockpit
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gptkbp:combat_radius
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600 km
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gptkbp:controls
|
rudder
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gptkbp:crew
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gptkb:1
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gptkbp:design
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gptkb:Yakovlev_design_bureau
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gptkbp:design_date
|
1945
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gptkbp:design_feature
|
high maneuverability
swept wings
high thrust-to-weight ratio
low drag design
trapezoidal wings
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gptkbp:engine
|
Klimov VK-105 PF
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gptkbp:first_flight
|
1947
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gptkbp:floors
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all-moving tailplane
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gptkbp:fuel_capacity
|
800 L
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gptkbp:fuselage_material
|
gptkb:NACA_0012
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gptkbp:height
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2.9 m
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|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-23
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gptkbp:introduced
|
1948
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gptkbp:landing_distance
|
150 km/h
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|
gptkbp:landing_gear
|
tricycle gear
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gptkbp:length
|
8.2 m
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gptkbp:manufacturer
|
gptkb:Yakovlev
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gptkbp:max_speed
|
900 km/h
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gptkbp:max_takeoff_weight
|
2,800 kg
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gptkbp:nickname
|
gptkb:gardens
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|
gptkbp:number_built
|
approximately 1,000
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gptkbp:operational_use
|
1948
1970s
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gptkbp:origin
|
gptkb:Soviet_Union
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gptkbp:propulsion
|
gptkb:jet_engine
|
|
gptkbp:range
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1,200 km
|
|
gptkbp:retired
|
1960s
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gptkbp:role
|
air superiority fighter
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gptkbp:roll_rate
|
high
ailerons
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gptkbp:service
|
gptkb:Egyptian_Air_Force
gptkb:Soviet_Air_Force
gptkb:Polish_Air_Force
gptkb:Hungarian_Air_Force
gptkb:Czechoslovak_Air_Force
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gptkbp:service_ceiling
|
12,000 m
|
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gptkbp:stall_speed
|
120 km/h
|
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gptkbp:strikeouts
|
elevators
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gptkbp:successor
|
Yakovlev Yak-25
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gptkbp:variant
|
gptkb:Yak-23_P
Yak-23 U
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|
gptkbp:weight
|
3,200 kg
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|
gptkbp:wing_area
|
16.5 m²
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gptkbp:wing_configuration
|
low-wing
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|
gptkbp:wingspan
|
8.5 m
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gptkbp:bfsParent
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gptkb:Shvetsov_ASh-82
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gptkbp:bfsLayer
|
6
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