Statements (34)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turboprop engine
|
| gptkbp:compressionRatio |
8:1
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:diameter |
1,200 mm
|
| gptkbp:engine |
2
|
| gptkbp:firstRace |
1955
|
| gptkbp:fuel_capacity |
0.5 kg/hp·h
|
| gptkbp:fuelType |
aviation kerosene
|
| https://www.w3.org/2000/01/rdf-schema#label |
NK-12 engine
|
| gptkbp:is_designed_to |
Kuznetsov
|
| gptkbp:is_used_in |
gptkb:Tupolev_Tu-95
gptkb:Tupolev_Tu-16 gptkb:Tupolev_Tu-95MS gptkb:Tupolev_Tu-95U gptkb:Tupolev_Tu-114 gptkb:Antonov_An-22 gptkb:Tupolev_Tu-95M gptkb:Ilyushin_Il-18 gptkb:Tupolev_Tu-95RTs Ilyushin Il-38 Tupolev Tu-95K Tupolev Tu-95N Tupolev Tu-95V Tupolev Tu-95MSM |
| gptkbp:length |
3,800 mm
|
| gptkbp:notable_feature |
reverse thrust capability
|
| gptkbp:operational_status |
military aircraft
civil aircraft |
| gptkbp:powerOutput |
15,000 hp
|
| gptkbp:produces |
gptkb:Soviet_Union
|
| gptkbp:propulsion |
5,000 lbf
|
| gptkbp:replacedBy |
NK-32 engine
|
| gptkbp:type |
aircraft engine
|
| gptkbp:weight |
1,200 kg
|