Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
1.15:1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.25 m
|
| gptkbp:firstFlight |
1963
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-8 engine
|
| gptkbp:length |
4.8 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:status |
out of production
|
| gptkbp:successor |
gptkb:NK-86_engine
|
| gptkbp:thrust |
90 kN
|
| gptkbp:type |
turbofan
|
| gptkbp:usedInAircraft |
gptkb:Ilyushin_Il-62
gptkb:Tupolev_Tu-154 |
| gptkbp:weight |
2,300 kg
|
| gptkbp:bfsParent |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:bfsLayer |
6
|