Statements (25)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
gptkb:piston_engine
|
| gptkbp:compressionRatio |
9.0:1
|
| gptkbp:configuration |
contra-rotating propellers
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.2 m
|
| gptkbp:enteredService |
1955
|
| gptkbp:firstFlight |
1952
|
| gptkbp:fuelType |
kerosene
|
| gptkbp:length |
5.4 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:notableFor |
most powerful turboprop engine in service
|
| gptkbp:numberOfEngines |
14
|
| gptkbp:numberOfStages |
14
5 |
| gptkbp:powerOutput |
up to 15,000 shp
|
| gptkbp:type |
axial-flow 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:A-90_Ekranoplan
gptkb:A-90_Orlyonok |
| gptkbp:bfsLayer |
7
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-12 turboprop
|