Statements (22)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
piston engine
|
| gptkbp:application |
bomber
supersonic transport |
| gptkbp:bypassRatio |
1.4:1
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:diameter |
1.46 m
|
| gptkbp:firstFlight |
1980s
|
| gptkbp:fuelType |
kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-32
|
| gptkbp:length |
6.1 m
|
| gptkbp:manufacturer |
gptkb:Kuznetsov_Design_Bureau
|
| gptkbp:relatedTo |
NK-25
|
| gptkbp:status |
in production
|
| gptkbp:successor |
NK-32-02
|
| gptkbp:thrust |
245 kN
|
| gptkbp:type |
afterburning turbofan
|
| gptkbp:usedInAircraft |
gptkb:Tupolev_Tu-160
Tupolev Tu-22M3M Tupolev Tu-144LL |
| gptkbp:weight |
3,400 kg
|
| gptkbp:bfsParent |
gptkb:NK32-4
|
| gptkbp:bfsLayer |
7
|