NK-12 engine

GPTKB entity

Statements (53)
Predicate Object
gptkbp:instance_of gptkb:turbofan_engine
gptkbp:application strategic bombers
gptkbp:average_temperature up to 800 ° C
gptkbp:compression_ratio 8:1
gptkbp:control_system mechanical control
gptkbp:cooling_system air-cooled
gptkbp:design_features high power-to-weight ratio
gptkbp:designed_by gptkb:Kuznetsov
gptkbp:development 1950s
gptkbp:diameter 1.5 m
gptkbp:emissions_standard moderate
gptkbp:engine gptkb:NK_family_of_engines
2
Brayton cycle
gptkbp:engine_configuration inline
gptkbp:fuel_economy 0.5 kg/hp·h
gptkbp:fuel_type aviation kerosene
gptkbp:historical_significance first turboprop engine with a power output over 10,000 hp
https://www.w3.org/2000/01/rdf-schema#label NK-12 engine
gptkbp:ignition_system spark ignition
gptkbp:influenced_by German engines from WWII
gptkbp:inspiration modern turboprop engines
gptkbp:involved_technology turbine technology
gptkbp:legacy used in various military aircraft
gptkbp:legal_principle gptkb:internal_combustion_engine
gptkbp:length 4.2 m
gptkbp:maintenance 1,000 hours
gptkbp:maximum_power_output 15,000 hp
gptkbp:noise_level high
gptkbp:notable_feature reverse thrust capability
gptkbp:notable_users gptkb:Soviet_Air_Force
gptkbp:number_of_engines gptkb:18
gptkbp:operational_history served in Cold War era
gptkbp:operational_range up to 10,000 m
gptkbp:original_run gptkb:1954
gptkbp:produced 1970s
gptkbp:produced_by gptkb:Soviet_Union
gptkbp:production_status out of production
gptkbp:propeller variable-pitch propeller
gptkbp:propulsion 12.5:1
gptkbp:related_aircraft gptkb:Tupolev_Tu-16
gptkb:Tupolev_Tu-95_K
gptkb:Tupolev_Tu-95_V
gptkb:Tupolev_Tu-95_MS
gptkb:Myasishchev_M-4
gptkbp:reliability high
gptkbp:successor gptkb:NK-16_engine
gptkbp:type gptkb:jet_engine
gptkbp:used_in gptkb:Tupolev_Tu-95
gptkb:Tupolev_Tu-114
gptkbp:weight 1,200 kg
gptkbp:bfsParent gptkb:Kuznetsov_Design_Bureau
gptkbp:bfsLayer 6