|
gptkbp:instance_of
|
gptkb:jet_engine
|
|
gptkbp:application
|
gptkb:military_aircraft
|
|
gptkbp:check_in_time
|
yes
|
|
gptkbp:combustor_type
|
annular
|
|
gptkbp:compression_ratio
|
8:1
|
|
gptkbp:control_system
|
hydraulic
|
|
gptkbp:cooling_system
|
gptkb:Interpol
air-cooled
|
|
gptkbp:design_date
|
gptkb:Cold_War
|
|
gptkbp:development
|
1950s to 1960s
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:engine
|
modular
aerodynamics research
Soviet aviation history
1960s technology
air-start
Kuznetsov design bureau
turbojet advancements
Kuznetsov NK-8-2
|
|
gptkbp:engine_compatibility_with
|
Tupolev Tu-16 K.
|
|
gptkbp:engine_configuration
|
gptkb:1
single-spool
wing-mounted
pylon-mounted
|
|
gptkbp:engine_impact_on_design
|
aircraft design evolution
|
|
gptkbp:engine_legacy_system
|
Soviet jet engines
|
|
gptkbp:engine_power
|
high thrust-to-weight ratio
|
|
gptkbp:engine_specification
|
military specifications
|
|
gptkbp:engine_technology_transfer
|
Cold War technology transfer
|
|
gptkbp:engine_type
|
gptkb:Tupolev_Tu-95
axial-flow
NK-8-2
|
|
gptkbp:first_flight
|
gptkb:1960
|
|
gptkbp:fuel_economy
|
0.85 kg/k N·h
|
|
gptkbp:fuel_type
|
kerosene
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kuznetsov NK-8-2 U
|
|
gptkbp:impact
|
strategic bomber capabilities
|
|
gptkbp:length
|
4,000 mm
|
|
gptkbp:maintenance
|
500 hours
ground maintenance
|
|
gptkbp:manufacturer
|
gptkb:Kuznetsov
|
|
gptkbp:noise_level
|
85 d B
|
|
gptkbp:number_of_stages
|
gptkb:5
|
|
gptkbp:operational_range
|
1,500 km
|
|
gptkbp:propulsion
|
no
8,000 lbf
|
|
gptkbp:related_aircraft
|
gptkb:Tupolev_family
|
|
gptkbp:reliability
|
0.95
|
|
gptkbp:service_ceiling
|
12,000 m
|
|
gptkbp:successor
|
Kuznetsov NK-12
|
|
gptkbp:type
|
gptkb:turbofan_engine
|
|
gptkbp:used_in
|
gptkb:Tupolev_Tu-16
|
|
gptkbp:weight
|
1,200 kg
|
|
gptkbp:bfsParent
|
gptkb:A-50
|
|
gptkbp:bfsLayer
|
7
|