|
gptkbp:instanceOf
|
jet engine
|
|
gptkbp:aircraft
|
Tupolev_Tu-144_family
|
|
gptkbp:application
|
civil aviation
|
|
gptkbp:controls
|
hydromechanical
|
|
gptkbp:coolingSystem
|
air-cooled
|
|
gptkbp:developer
|
gptkb:Soviet_Union
|
|
gptkbp:diameter
|
1,200 mm
|
|
gptkbp:emissionsStandard
|
non-compliant
|
|
gptkbp:engine
|
2
rear-mounted
|
|
gptkbp:engineConfiguration
|
twin-shaft
|
|
gptkbp:engineType
|
compressed air
axial
single-stage
NK-144A
NK-144C
NK-144D
NK-144E
NK-144G
NK-144H
NK-144I
NK-144K
NK-144M
NK-144P
NK-144R
NK-144S
NK-144T
NK-144U
NK-144V
NK-144Z
NK-144B
NK-144F
NK-144J
NK-144L
NK-144N
NK-144O
NK-144Q
NK-144W
NK-144X
NK-144Y
|
|
gptkbp:exhaustSystem
|
variable geometry
|
|
gptkbp:firstFlight
|
1970
|
|
gptkbp:fuel_capacity
|
1,200 kg/h
0.9 kg/kgf·h
|
|
gptkbp:fuelType
|
annular
spark plug
kerosene
|
|
gptkbp:hasArea
|
gptkb:Kuznetsov_plant
Soviet_certification
|
|
https://www.w3.org/2000/01/rdf-schema#label
|
Kuznetsov NK-144
|
|
gptkbp:is_used_in
|
gptkb:Tupolev_Tu-144
|
|
gptkbp:length
|
4,200 mm
|
|
gptkbp:maintenance
|
1,000 hours
|
|
gptkbp:manufacturer
|
Kuznetsov
|
|
gptkbp:maximum_speed
|
2,500 km/h
|
|
gptkbp:noise_level
|
high
|
|
gptkbp:operational_status
|
1970s
|
|
gptkbp:operationalRange
|
6,000 km
|
|
gptkbp:propulsion
|
11.67
14,000 kgf
|
|
gptkbp:related_engine
|
Brayton_cycle
|
|
gptkbp:service_ceiling
|
15,000 m
|
|
gptkbp:successor
|
gptkb:Kuznetsov_NK-321
|
|
gptkbp:team
|
gptkb:A.S._Kuznetsov
|
|
gptkbp:type
|
afterburning turbojet engine
|
|
gptkbp:weight
|
1,200 kg
|