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gptkbp:instance_of
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gptkb:aircraft
|
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gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:An-70
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|
gptkbp:aircraft_operated
|
gptkb:An-124_Ruslan
fixed-wing aircraft
high-wing
Antonov An family
|
|
gptkbp:avionics
|
modern digital
|
|
gptkbp:capacity
|
up to 47,000 kg
|
|
gptkbp:crew
|
gptkb:5
|
|
gptkbp:design
|
gptkb:Antonov_Design_Bureau
gptkb:Company
twin-engine
|
|
gptkbp:developer
|
gptkb:1980s
gptkb:An-70
|
|
gptkbp:emergency_services
|
multiple exits
|
|
gptkbp:engine
|
D-27
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:exported_to
|
gptkb:Russia
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:first_released
|
gptkb:2000
|
|
gptkbp:fuel_capacity
|
40,000 L
|
|
gptkbp:height
|
10.5 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
An-70 M
|
|
gptkbp:interior_features
|
modular
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
30.3 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
700 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 m
1,000 m
120,000 kg
|
|
gptkbp:military_branch
|
gptkb:An-70
|
|
gptkbp:military_technology
|
gptkb:An-70_T
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
|
gptkbp:number_built
|
approximately 20
|
|
gptkbp:operational_history
|
limited
|
|
gptkbp:operational_range
|
1,500 km with max payload
|
|
gptkbp:origin
|
gptkb:Ukraine
|
|
gptkbp:primary_user
|
gptkb:Ukrainian_Air_Force
|
|
gptkbp:production_years
|
1994-present
|
|
gptkbp:propulsion
|
six-blade
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:role
|
gptkb:public_transportation_system
|
|
gptkbp:seating_capacity
|
automated systems
rear ramp
200 m³
large volume for military equipment
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:speed
|
600 km/h
|
|
gptkbp:status
|
in service
|
|
gptkbp:stealth_features
|
limited
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
150 m²
|
|
gptkbp:wingspan
|
44.5 m
|