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gptkbp:instance_of
|
gptkb:aircraft
|
|
gptkbp:bfsLayer
|
5
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gptkbp:bfsParent
|
gptkb:An-70
|
|
gptkbp:aircraft_operated
|
gptkb:aircraft
gptkb:An-12
gptkb:An-22
gptkb:An-124
high-wing
|
|
gptkbp:armament
|
gptkb:none
|
|
gptkbp:avionics
|
modern
|
|
gptkbp:budget
|
gptkb:unknown
|
|
gptkbp:combat_role
|
gptkb:Company
|
|
gptkbp:community_role
|
cargo transport
|
|
gptkbp:crew
|
gptkb:5
|
|
gptkbp:design
|
gptkb:Antonov_Design_Bureau
gptkb:patent
twin-boom
replace An-12
|
|
gptkbp:developer
|
gptkb:unknown
1990s
|
|
gptkbp:engine
|
gptkb:4
Ivchenko-Progress
|
|
gptkbp:engine_type
|
gptkb:AI-20_M
turboprop
|
|
gptkbp:exported_to
|
gptkb:none
|
|
gptkbp:first_flight
|
gptkb:1994
|
|
gptkbp:fuel_capacity
|
20,000 L
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
An-70 A
|
|
gptkbp:influenced_by
|
gptkb:An-70
|
|
gptkbp:invention
|
gptkb:1994
|
|
gptkbp:landing_gear
|
tricycle gear
|
|
gptkbp:length
|
30.3 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:material
|
3.5 m
aluminum alloy
|
|
gptkbp:max_speed
|
700 km/h
|
|
gptkbp:max_takeoff_weight
|
1,200 m
1,000 m
120,000 kg
|
|
gptkbp:military_technology
|
gptkb:none
|
|
gptkbp:notable_features
|
short takeoff and landing
|
|
gptkbp:operational_area
|
2000s
|
|
gptkbp:operational_history
|
limited use
|
|
gptkbp:predecessor
|
gptkb:none
|
|
gptkbp:primary_user
|
gptkb:Ukrainian_Air_Force
|
|
gptkbp:produced_by
|
limited
|
|
gptkbp:range
|
2,500 km
|
|
gptkbp:role
|
gptkb:aircraft
|
|
gptkbp:seating_capacity
|
70
rear ramp
60 m³
47,000 kg
|
|
gptkbp:service_ceiling
|
10,000 m
|
|
gptkbp:speed
|
650 km/h
|
|
gptkbp:status
|
in development
|
|
gptkbp:successor
|
gptkb:none
|
|
gptkbp:tail_type
|
T-tail
|
|
gptkbp:wing_area
|
150 m²
|
|
gptkbp:wingspan
|
44.5 m
|