Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
axial flow
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Alexander_Ivchenko
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:firstFlight |
1955
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-20
|
| gptkbp:length |
3.1 m
|
| gptkbp:manufacturer |
Ivchenko OKB
|
| gptkbp:numberOfEngines |
none
|
| gptkbp:powerOutput |
4,000 shp
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Ivchenko_AI-24
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Antonov_An-12
gptkb:Beriev_Be-12 gptkb:Ilyushin_Il-18 gptkb:Ilyushin_Il-20 gptkb:Ilyushin_Il-22 gptkb:Antonov_An-10 |
| gptkbp:weight |
1,050 kg
|
| gptkbp:bfsParent |
gptkb:An-32
|
| gptkbp:bfsLayer |
6
|