Statements (17)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:bypassRatio |
2.6:1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.5 m
|
| gptkbp:engineType |
turbofan
|
| gptkbp:firstFlight |
1987
|
| gptkbp:fuelType |
kerosene
liquid hydrogen |
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-87
|
| gptkbp:length |
5.5 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:status |
out of production
|
| gptkbp:thrust |
127.4 kN
|
| gptkbp:usedInAircraft |
gptkb:Lun-class_ekranoplan
|
| gptkbp:weight |
3,500 kg
|
| gptkbp:bfsParent |
gptkb:Kuznetsov_NK-86_turbofan
|
| gptkbp:bfsLayer |
6
|