Statements (31)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:configuration |
axial-flow
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:enteredService |
1955
|
| gptkbp:firstFlight |
1952
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-12
|
| gptkbp:length |
5.4 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:maximumSpeed |
8,000
|
| gptkbp:notableFor |
most powerful turboprop engine in service
|
| gptkbp:numberOfAxles |
two
|
| gptkbp:numberOfEngines |
none
|
| gptkbp:numberOfStages |
14
6 |
| gptkbp:powerOutput |
up to 15,000 shp
|
| gptkbp:propulsion |
contra-rotating
|
| gptkbp:type |
turboprop
|
| 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:Tupolev_Tu-114
gptkb:Tupolev_Tu-142 gptkb:Tu-142 gptkb:Ту-95 gptkb:Tu-95 |
| gptkbp:bfsLayer |
6
|