Statements (24)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
two-shaft
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Oleksandr_Ivchenko
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:firstFlight |
1960
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-24
|
| gptkbp:introduced |
1960s
|
| gptkbp:length |
2.5 m
|
| gptkbp:manufacturer |
gptkb:Ivchenko-Progress
|
| gptkbp:numberOfEngines |
nan
|
| gptkbp:powerOutput |
2,820 shp
|
| gptkbp:status |
in service
|
| gptkbp:successor |
gptkb:Ivchenko_AI-20
|
| gptkbp:type |
turboprop
|
| gptkbp:usedInAircraft |
gptkb:Antonov_An-24
gptkb:Antonov_An-26 gptkb:Antonov_An-32 gptkb:Antonov_An-30 |
| gptkbp:weight |
750 kg
|
| gptkbp:bfsParent |
gptkb:Antonov_An-24
gptkb:An-24 |
| gptkbp:bfsLayer |
6
|