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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:Yak-11_M
gptkb:Yak-18
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gptkbp:aircraft_operated
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gptkb:aircraft
gptkb:Yak-52
gptkb:item
manual control
straight wing
Valery Chkalov
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gptkbp:armament
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gptkb:none
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gptkbp:cockpit
|
open cockpit
single-seat
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gptkbp:crew
|
gptkb:musical
|
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gptkbp:design
|
gptkb:Yakovlev_Design_Bureau
low-wing monoplane
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gptkbp:engine
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gptkb:Vedeneyev_M14_P
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gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:first_flight
|
gptkb:1975
high
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|
gptkbp:flaps
|
split flaps
|
|
gptkbp:floors
|
conventional tail
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|
gptkbp:fuel_capacity
|
200 L
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gptkbp:height
|
2.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yak-50
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gptkbp:introduced
|
gptkb:1975
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|
gptkbp:is_designed_to
|
training and aerobatics
|
|
gptkbp:is_used_by
|
aerobatic teams
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.2 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:material
|
gptkb:item
all-metal construction
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
90 km/h
400 m
1,200 kg
|
|
gptkbp:number_built
|
approximately 200
|
|
gptkbp:origin
|
gptkb:Monarch
|
|
gptkbp:power_output
|
360 hp
|
|
gptkbp:primary_user
|
aerobatic teams
|
|
gptkbp:production_years
|
gptkb:1980s
gptkb:1975
|
|
gptkbp:propulsion
|
two-bladed propeller
|
|
gptkbp:range
|
600 km
|
|
gptkbp:retired
|
1990s
|
|
gptkbp:role
|
aerobatic aircraft
|
|
gptkbp:roll_rate
|
360°/s
|
|
gptkbp:service_ceiling
|
3,000 m
|
|
gptkbp:setting
|
single-engine
|
|
gptkbp:speed
|
80 km/h
good
|
|
gptkbp:successor
|
gptkb:Yak-52
|
|
gptkbp:surface
|
full-span ailerons
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:training
|
aerobatic training
|
|
gptkbp:type
|
civil aircraft
|
|
gptkbp:variant
|
Yak-50 M
|
|
gptkbp:wing_area
|
14.5 m²
|
|
gptkbp:wingspan
|
9.5 m
|