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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
4
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gptkbp:bfsParent
|
gptkb:Soviet_Air_Forces
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:An-124_Ruslan
gptkb:An-225_Mriya
high-wing
twin-engine turboprop
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|
gptkbp:avionics
|
modern digital
|
|
gptkbp:combat_role
|
freight transport
airlift
|
|
gptkbp:crew
|
gptkb:5
|
|
gptkbp:design
|
gptkb:Antonov_Design_Bureau
gptkb:Company
|
|
gptkbp:developer
|
$300 million
1980s to 1990s
|
|
gptkbp:engine
|
gptkb:4
D-27
|
|
gptkbp:engine_type
|
turboprop
|
|
gptkbp:features
|
high lift devices
|
|
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
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
30.3 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:max_speed
|
700 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 m
800 m
120,000 kg
|
|
gptkbp:notable_features
|
short takeoff and landing capabilities
|
|
gptkbp:operational_area
|
gptkb:1999
|
|
gptkbp:operational_range
|
1,500 km with maximum payload
|
|
gptkbp:primary_user
|
gptkb:Ukrainian_Air_Force
Russia, Ukraine, Kazakhstan
|
|
gptkbp:produced_by
|
in production
|
|
gptkbp:production_location
|
gptkb:Ukraine
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:safety_features
|
good
|
|
gptkbp:seating_capacity
|
70
30,000 kg
rear ramp
47,000 kg
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:variant
|
gptkb:An-70_A
gptkb:An-70_M
gptkb:An-70_T
|
|
gptkbp:wing_area
|
150 m²
|
|
gptkbp:wingspan
|
44.5 m
|