Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:category |
gptkb:piston_engine
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Oleksandr_Ivchenko
|
| gptkbp:diameter |
1.1 m
|
| gptkbp:firstFlight |
1950s
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
3.1 m
|
| gptkbp:manufacturer |
Ivchenko Progress
|
| gptkbp:numberOfAxles |
two
|
| gptkbp:numberOfEngines |
none (turboprop)
|
| gptkbp:powerOutput |
4,250 shp
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Ivchenko_AI-24
|
| gptkbp:usedInAircraft |
gptkb:Antonov_An-12
gptkb:Ilyushin_Il-18 gptkb:Antonov_An-10 Ilyushin Il-20M |
| gptkbp:weight |
1,050 kg
|
| gptkbp:bfsParent |
gptkb:Ilyushin_Il-18D
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-20M turboprop
|