Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:compressionRatio |
axial-flow
|
| gptkbp:configuration |
contra-rotating propellers
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.3 m
|
| gptkbp:firstFlight |
1952
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-12 engine
|
| gptkbp:length |
5.4 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:maximumSpeed |
8,800
|
| gptkbp:notableFor |
most powerful turboprop engine in service
|
| gptkbp:numberOfEngines |
14
|
| gptkbp:powerOutput |
15,000 shp
|
| gptkbp:relatedTo |
Junkers Jumo 022
|
| gptkbp:usedIn |
gptkb:aircraft
|
| gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-114
gptkb:Antonov_An-22 gptkb:Tupolev_Tu-142 gptkb:Tupolev_Tu-95 |
| gptkbp:weight |
2,900 kg
|
| gptkbp:bfsParent |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:bfsLayer |
6
|