Statements (21)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
civil aviation
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.46 m
|
| gptkbp:engineType |
low-bypass turbofan
|
| gptkbp:firstFlight |
1974
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-86
|
| gptkbp:length |
4.84 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:notableFeature |
first Soviet high-bypass turbofan for civil use
|
| gptkbp:numberOfAxles |
two
|
| gptkbp:numberOfStages |
13
3 |
| gptkbp:status |
out of production
|
| gptkbp:successor |
Kuznetsov NK-92
|
| gptkbp:thrust |
127.5 kN
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-86
|
| gptkbp:weight |
3,900 kg
|
| gptkbp:bfsParent |
gptkb:Kuznetsov_NK-8
|
| gptkbp:bfsLayer |
7
|