Statements (19)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:afterburning |
yes
|
| gptkbp:application |
gptkb:aircraft
|
| gptkbp:bypassRatio |
2.0
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.46 m
|
| gptkbp:firstFlight |
1971
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-25
|
| gptkbp:length |
6.1 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:relatedTo |
gptkb:Kuznetsov_NK-32
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
245 kN
|
| gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-22M
Tupolev Tu-160 (prototype) |
| gptkbp:weight |
2,500 kg
|
| gptkbp:bfsParent |
gptkb:2_×_Kuznetsov_NK-25_turbofan_engines
|
| gptkbp:bfsLayer |
7
|