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gptkbp:instance_of
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gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:Antonov
gptkb:Airbus_A400_family
|
|
gptkbp:aircraft_operated
|
gptkb:Antonov_family
gptkb:aircraft
gptkb:Company
gptkb:Antonov_An-225
gptkb:Antonov_An-124
fixed-wing aircraft
multirole
high-wing
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|
gptkbp:avionics
|
modern digital
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|
gptkbp:crew
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gptkb:5
2 pilots
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|
gptkbp:design
|
gptkb:Antonov_Design_Bureau
gptkb:Oleg_Antonov
strategic airlift
replace An-12
|
|
gptkbp:developer
|
1980s to 1990s
|
|
gptkbp:engine
|
gptkb:4
|
|
gptkbp:engine_type
|
turbofan
D-27
|
|
gptkbp:features
|
short takeoff and landing
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:first_released
|
not completed
|
|
gptkbp:historical_event
|
developed for Soviet military needs
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antonov An-70
|
|
gptkbp:length
|
30.3 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:max_speed
|
800 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:none
|
|
gptkbp:notable_feature
|
high lift devices
|
|
gptkbp:operational_area
|
limited to testing
|
|
gptkbp:operational_range
|
1,500 km with maximum payload
|
|
gptkbp:origin
|
gptkb:Ukraine
|
|
gptkbp:primary_user
|
gptkb:Ukrainian_Air_Force
|
|
gptkbp:produced_by
|
limited production
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:role
|
airlift
|
|
gptkbp:seating_capacity
|
up to 300
60,000 kg
rear ramp
47,000 kg
200 m³
onboard loading system
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:status
|
gptkb:patent
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
200 m²
|
|
gptkbp:wingspan
|
44.5 m
|