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gptkbp:instanceOf
|
gptkb:aircraft
|
|
gptkbp:avionics
|
glass cockpit
|
|
gptkbp:cabinWidth
|
4.0 m
|
|
gptkbp:capacity
|
47,000 kg
|
|
gptkbp:cargoHoldHeight
|
4.1 m
|
|
gptkbp:cargoHoldLength
|
19.1 m
|
|
gptkbp:carries
|
gptkb:aircraft
troops
paratroopers
cargo pallets
|
|
gptkbp:constructionStartYear
|
1980s
|
|
gptkbp:contrastsWith
|
gptkb:Airbus_A400M
gptkb:Lockheed_C-130J_Super_Hercules
|
|
gptkbp:countryOfOrigin
|
gptkb:Ukraine
|
|
gptkbp:crew
|
4
|
|
gptkbp:engine
|
gptkb:Progress_D-27
|
|
gptkbp:engineType
|
propfan
|
|
gptkbp:firstFlight
|
gptkb:Kyiv,_Ukraine
1994
|
|
gptkbp:firstPrototypeCrash
|
1995
|
|
gptkbp:fuelType
|
38,000 kg
|
|
gptkbp:height
|
16.38 m
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Antonov An-70
|
|
gptkbp:landingGear
|
retractable tricycle
|
|
gptkbp:length
|
40.7 m
|
|
gptkbp:manufacturer
|
gptkb:Antonov
|
|
gptkbp:material
|
aluminum alloy
|
|
gptkbp:maximumSpeed
|
780 km/h
|
|
gptkbp:maxTakeoffWeight
|
132,000 kg
|
|
gptkbp:notableEvent
|
1995 mid-air collision
|
|
gptkbp:notableFeature
|
propfan engines
short takeoff and landing capability
|
|
gptkbp:notableProject
|
limited production
|
|
gptkbp:numberBuilt
|
2
|
|
gptkbp:numberOfAxles
|
high-wing
|
|
gptkbp:numberOfEngines
|
4
|
|
gptkbp:paratroopDoors
|
yes
|
|
gptkbp:partner
|
gptkb:Russia
gptkb:Ukraine
|
|
gptkbp:pressurizedCabin
|
yes
|
|
gptkbp:primaryUser
|
gptkb:Ukrainian_Air_Force
|
|
gptkbp:rampDoor
|
yes
|
|
gptkbp:rangeWithMaxFuel
|
8,000 km
|
|
gptkbp:rangeWithMaxPayload
|
3,000 km
|
|
gptkbp:role
|
medium-range transport
|
|
gptkbp:status
|
gptkb:prototype
|
|
gptkbp:successor
|
gptkb:Antonov_An-12
|
|
gptkbp:tailLength
|
T-tail
|
|
gptkbp:targetMarket
|
gptkb:CIS_countries
|
|
gptkbp:wingspan
|
44.06 m
|
|
gptkbp:bfsParent
|
gptkb:Antonov
|
|
gptkbp:bfsLayer
|
5
|