Statements (24)
Predicate | Object |
---|---|
gptkbp:instanceOf |
piston engine
|
gptkbp:bypassRatio |
1.4:1
|
gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
gptkbp:diameter |
1.46 m
|
gptkbp:firstFlight |
1980
|
gptkbp:fuelType |
kerosene
|
https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-32
|
gptkbp:length |
6.1 m
|
gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
gptkbp:notableFeature |
most powerful afterburning turbofan in production
|
gptkbp:numberOfAxles |
3
|
gptkbp:numberOfStages |
2 low-pressure, 1 high-pressure
3 low-pressure, 5 high-pressure |
gptkbp:status |
in service
|
gptkbp:successor |
Kuznetsov NK-65
|
gptkbp:thrust |
245 kN
|
gptkbp:type |
afterburning turbofan
|
gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-160
Tupolev Tu-22M3 Tupolev Tu-144LL |
gptkbp:weight |
3,400 kg
|
gptkbp:bfsParent |
gptkb:Tu-160M2
gptkb:Tu-160_bomber_engines |
gptkbp:bfsLayer |
7
|