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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
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|
gptkbp:bfsParent
|
gptkb:Mikulin
|
|
gptkbp:aircraft_operated
|
single-engine
low-wing
|
|
gptkbp:armament
|
2 × 12.7 mm UBS machine guns
1 × 23 mm Nudelman-Suranov NS-23 cannon
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|
gptkbp:climb_rate
|
20 m/s
|
|
gptkbp:cockpit
|
enclosed cockpit
|
|
gptkbp:combat_radius
|
600 km
|
|
gptkbp:controls
|
rudder
|
|
gptkbp:crew
|
gptkb:musical
|
|
gptkbp:date
|
1945
|
|
gptkbp:design
|
gptkb:Yakovlev_design_bureau
|
|
gptkbp:engine
|
Klimov VK-105 PF
|
|
gptkbp:features
|
high maneuverability
swept wings
high thrust-to-weight ratio
low drag design
trapezoidal wings
|
|
gptkbp:first_flight
|
1947
|
|
gptkbp:floors
|
all-moving tailplane
|
|
gptkbp:fuel_capacity
|
800 L
|
|
gptkbp:height
|
2.9 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-23
|
|
gptkbp:introduced
|
1948
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:material
|
gptkb:NACA_0012
|
|
gptkbp:max_speed
|
900 km/h
|
|
gptkbp:max_takeoff_weight
|
150 km/h
2,800 kg
|
|
gptkbp:nickname
|
gptkb:physicist
|
|
gptkbp:number_built
|
approximately 1,000
|
|
gptkbp:operational_area
|
1948
1970s
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:propulsion
|
gptkb:engine
|
|
gptkbp:range
|
1,200 km
|
|
gptkbp:retired
|
1960s
|
|
gptkbp:role
|
air superiority fighter
|
|
gptkbp:roll_rate
|
high
ailerons
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:services
|
gptkb:Egyptian_Air_Force
gptkb:Soviet_Air_Force
gptkb:Polish_Air_Force
gptkb:Hungarian_Air_Force
gptkb:Czechoslovak_Air_Force
|
|
gptkbp:speed
|
120 km/h
|
|
gptkbp:strikeouts
|
elevators
|
|
gptkbp:successor
|
Yakovlev Yak-25
|
|
gptkbp:variant
|
gptkb:Yak-23_P
Yak-23 U
|
|
gptkbp:weight
|
3,200 kg
|
|
gptkbp:wing_area
|
16.5 m²
|
|
gptkbp:wingspan
|
8.5 m
|