|
gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
7
|
|
gptkbp:bfsParent
|
gptkb:Yakovlev_Yak-14
gptkb:Mikulin
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:Yakovlev_Yak-50
gptkb:Yakovlev_Yak-70
gptkb:Yakovlev_Yak-80
gptkb:Yakovlev_Yak-90
composite materials
civilian trainer
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:aspect_ratio
|
6.3
|
|
gptkbp:climb_rate
|
10 m/s
|
|
gptkbp:cockpit
|
two-seat tandem
|
|
gptkbp:combat_role
|
pilot training
|
|
gptkbp:crew
|
2
|
|
gptkbp:design
|
gptkb:Yakovlev_Design_Bureau
low-wing monoplane
|
|
gptkbp:engine
|
gptkb:Klimov_VK-1
|
|
gptkbp:engine_type
|
gptkb:engine
|
|
gptkbp:features
|
low drag design
|
|
gptkbp:first_flight
|
gptkb:1970
1970-06-01
1985-12-31
|
|
gptkbp:fuel_capacity
|
300 L
|
|
gptkbp:height
|
2.5 m
|
|
gptkbp:historical_significance
|
early jet trainer
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Yakovlev Yak-60
|
|
gptkbp:introduced
|
gptkb:1970
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
8.5 m
|
|
gptkbp:manufacturer
|
gptkb:Yakovlev
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
300 km/h
|
|
gptkbp:max_takeoff_weight
|
300 m
400 m
1,500 kg
|
|
gptkbp:number_built
|
50
|
|
gptkbp:primary_user
|
gptkb:Soviet_Air_Force
|
|
gptkbp:production_location
|
gptkb:Russia
|
|
gptkbp:production_years
|
1970-1980
|
|
gptkbp:propulsion
|
gptkb:engine
|
|
gptkbp:range
|
1,000 km
|
|
gptkbp:retired
|
gptkb:1980s
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:roll_rate
|
4.5°/s
|
|
gptkbp:service_ceiling
|
5,000 m
|
|
gptkbp:speed
|
80 km/h
|
|
gptkbp:successor
|
gptkb:Yakovlev_Yak-52
|
|
gptkbp:surface
|
gptkb:public_transportation_system
rudder
aileron
|
|
gptkbp:variant
|
Yak-60 A
|
|
gptkbp:wing_area
|
15 m²
|
|
gptkbp:wingspan
|
9.5 m
|