Statements (23)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
bomber
|
| gptkbp:bypassRatio |
1.4:1
|
| gptkbp:category |
military aircraft engine
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.46 m
|
| gptkbp:firstFlight |
1986
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-321 engine
|
| gptkbp:length |
6.1 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:numberOfStages |
2-stage high-pressure, 2-stage low-pressure
3-stage fan, 5-stage low-pressure, 6-stage high-pressure |
| gptkbp:relatedTo |
NK-25 engine
|
| gptkbp:status |
in service
|
| gptkbp:thrust |
245 kN
137 kN |
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-160
Tupolev Tu-22M3M |
| gptkbp:weight |
3,600 kg
|
| gptkbp:bfsParent |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:bfsLayer |
6
|