|
gptkbp:instanceOf
|
turbofan engine
|
|
gptkbp:aircraft
|
gptkb:Tupolev_family
|
|
gptkbp:application
|
military aircraft
|
|
gptkbp:climate
|
high temperature
|
|
gptkbp:compressionRatio
|
3.0
|
|
gptkbp:controls
|
digital control system
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:criticalReception
|
30:1
|
|
gptkbp:design_feature
|
modular design
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:emissionsStandard
|
low emissions
|
|
gptkbp:engine
|
extensive research and development
pylon-mounted
legacy in aviation history
Soviet_technology
|
|
gptkbp:engineConfiguration
|
twin-engine
|
|
gptkbp:engineType
|
axial
air start
advanced features for its time
several variants developed
|
|
gptkbp:firstRace
|
1967
|
|
gptkbp:fuel_capacity
|
high fuel efficiency
0.85 lb/hp/hr
|
|
gptkbp:fuelType
|
annular
kerosene
|
|
gptkbp:hasArea
|
certified for military use
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kuznetsov NK-32
|
|
gptkbp:is_used_in
|
gptkb:Tupolev_Tu-160
|
|
gptkbp:length
|
4,200 mm
|
|
gptkbp:maintenance
|
long maintenance interval
|
|
gptkbp:manufacturer
|
Kuznetsov
|
|
gptkbp:noise_level
|
low
advanced noise reduction technology
|
|
gptkbp:notableUsers
|
gptkb:Russian_Air_Force
|
|
gptkbp:number_of_stages
|
8
|
|
gptkbp:operational_status
|
in service
|
|
gptkbp:operationalRange
|
long-range
|
|
gptkbp:performances
|
high performance
|
|
gptkbp:produces
|
over 1,000 units
|
|
gptkbp:productionYears
|
1960s
1967-1990s
|
|
gptkbp:propulsion
|
25,000 lbf
no thrust vectoring
|
|
gptkbp:related_engine
|
gptkb:Kuznetsov_NK-25
|
|
gptkbp:reliability
|
high reliability
|
|
gptkbp:successor
|
gptkb:Kuznetsov_NK-321
|
|
gptkbp:team
|
gptkb:Kuznetsov_design_bureau
|
|
gptkbp:type
|
afterburning turbofan
|
|
gptkbp:weight
|
1,500 kg
|