gptkbp:instance_of
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gptkb:aircraft
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gptkbp:aircraft_configuration
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gptkb:ship
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gptkbp:aircraft_operated
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heavy transport aircraft
|
gptkbp:aircraft_role
|
strategic airlift
|
gptkbp:aircraft_type
|
gptkb:transport_aircraft
|
gptkbp:aspect_ratio
|
8.0
|
gptkbp:avionics
|
analog
|
gptkbp:built
|
gptkb:66
|
gptkbp:cargo_capacity
|
45,000 kg
|
gptkbp:cargo_types
|
3 m
30 m
4 m
3.5 m x 3.5 m
|
gptkbp:climb_rate
|
6 m/s
|
gptkbp:country_of_origin
|
gptkb:Soviet_Union
|
gptkbp:crew
|
gptkb:5
|
gptkbp:cruise_speed
|
600 km/h
|
gptkbp:decommissioned
|
gptkb:2000
|
gptkbp:design
|
gptkb:military_logistics
gptkb:Oleg_Antonov
|
gptkbp:design_features
|
high-wing design
|
gptkbp:engine_power
|
4,000 hp
|
gptkbp:engine_type
|
gptkb:Ivchenko_AI-20_M
turboprop
|
gptkbp:first_flight
|
gptkb:Kyiv
1965-02-27
|
gptkbp:fuel_capacity
|
40,000 L
|
gptkbp:height
|
12.5 m
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antonov An-22
|
gptkbp:landing_distance
|
1,200 m
200,000 lb
|
gptkbp:landing_gear
|
tricycle gear
|
gptkbp:length
|
57.3 m
|
gptkbp:manufacturer
|
gptkb:Antonov
|
gptkbp:max_speed
|
650 km/h
700 km/h
|
gptkbp:max_takeoff_weight
|
250,000 lb
|
gptkbp:notable_users
|
gptkb:Aeroflot
|
gptkbp:number_of_engines
|
gptkb:4
|
gptkbp:operational_range
|
4,000 km
|
gptkbp:passenger_capacity
|
60
|
gptkbp:payload_capacity
|
60,000 kg
|
gptkbp:production_years
|
1965-1986
|
gptkbp:propeller
|
variable-pitch
|
gptkbp:range
|
5,000 km
|
gptkbp:retired
|
gptkb:2000
|
gptkbp:role
|
gptkb:transport_aircraft
|
gptkbp:service
|
30 years
|
gptkbp:service_ceiling
|
10,000 m
|
gptkbp:successor
|
gptkb:Antonov_An-124
|
gptkbp:tail_type
|
T-tail
|
gptkbp:takeoff_distance
|
1,500 m
|
gptkbp:used_by
|
gptkb:Soviet_Air_Force
|
gptkbp:variant
|
gptkb:An-22_A
|
gptkbp:wing_area
|
400 m²
|
gptkbp:wing_configuration
|
high-wing
|
gptkbp:wingspan
|
64.4 m
|
gptkbp:year_established
|
gptkb:1965
|
gptkbp:bfsParent
|
gptkb:Antonov_Airlines
gptkb:Volga-Dnepr_Airlines
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gptkbp:bfsLayer
|
6
|