Properties (59)
| Predicate | Object |
|---|---|
| gptkbp:instanceOf |
turbofan engine
|
| gptkbp:airlines |
150 kg/s
|
| gptkbp:application |
military aviation
|
| gptkbp:controls |
hydromechanical
|
| gptkbp:coolingSystem |
air-cooled
|
| gptkbp:countryOfOrigin |
gptkb:Soviet_Union
|
| gptkbp:design |
advanced engineering techniques
high durability performance optimization safety features user-friendly interface advanced materials state-of-the-art technology cost-effectiveness environmental considerations reliable operation modular construction extensive testing high bypass ratio comprehensive documentation high thrust-to-weight ratio reduced drag afterburner low maintenance requirements efficient fuel consumption robust performance modular upgrades high thrust output sophisticated aerodynamics |
| gptkbp:designedBy |
Kuznetsov
|
| gptkbp:diameter |
1.3 m
|
| gptkbp:emissionsStandard |
moderate
|
| gptkbp:energyEfficiency |
moderate
|
| gptkbp:engineConfiguration |
twin-engine
|
| gptkbp:engineType |
2
4 afterburning turbofan |
| gptkbp:firstFlight |
1970
|
| gptkbp:fuelType |
annular
kerosene |
| gptkbp:hasContent |
0.85 kg/(kN·h)
|
| https://www.w3.org/2000/01/rdf-schema#label |
Kuznetsov NK-25
|
| gptkbp:introduced |
1970s
|
| gptkbp:length |
4.1 m
|
| gptkbp:maintenance |
1,000 hours
|
| gptkbp:noise_level |
high
|
| gptkbp:notableUsers |
gptkb:Soviet_Air_Force
gptkb:Russian_Air_Force |
| gptkbp:operationalRange |
varies by aircraft
|
| gptkbp:operationalStatus |
high
|
| gptkbp:productionCompany |
1960s to 1970s
|
| gptkbp:propulsion |
no
25,000 lbf |
| gptkbp:reliability |
high
|
| gptkbp:successor |
gptkb:Kuznetsov_NK-32
|
| gptkbp:type |
dual-spool
|
| gptkbp:usedIn |
gptkb:Tupolev_Tu-95
gptkb:Tupolev_Tu-160 |
| gptkbp:weight |
1,200 kg
|