Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:configuration |
twin-shaft
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:designer |
gptkb:Oleksandr_Ivchenko
|
| gptkbp:diameter |
0.9 m
|
| gptkbp:firstFlight |
1960
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
2.9 m
|
| gptkbp:manufacturer |
Ivchenko
|
| gptkbp:numberOfStages |
10
3 |
| gptkbp:powerOutput |
1900-2820 shp
|
| gptkbp:status |
in service
|
| gptkbp:successor |
Progress AI-20
|
| gptkbp:usedInAircraft |
gptkb:Antonov_An-24
gptkb:Antonov_An-26 gptkb:Antonov_An-32 gptkb:Antonov_An-30 |
| gptkbp:weight |
560 kg
|
| gptkbp:bfsParent |
gptkb:An-24B
|
| gptkbp:bfsLayer |
8
|
| https://www.w3.org/2000/01/rdf-schema#label |
Ivchenko AI-24 turboprop
|